Fluid Mechanics (XE-B) - GATE XE (Engineering Sciences) Subject-Wise PYQ Practice

Practice topic-wise Fluid Mechanics (XE-B) previous year questions for GATE XE (Engineering Sciences) with the official answer key. Step-by-step explanations are coming soon.

All GATE XE (Engineering Sciences) papers

292 questions. Answers are shown only where the official answer key is available.

Question 1

Year: 2025 | Marks: 1

Fluid at a constant flow rate passes through a long, straight, cylindrical pipe that has an axisymmetric convergent section at the end. Which one of the following options correctly represents the velocity field in the converging section in cylindrical (𝑟, 𝜃, 𝑧) coordinates?

  • A. Two-dimensional function of 𝑟 and 𝑧
  • B. One-dimensional function of 𝑟
  • C. Two-dimensional function of 𝑟 and 𝜃
  • D. One-dimensional function of 𝑧

Answer: A. Two-dimensional function of 𝑟 and 𝑧

Question 2

Year: 2025 | Marks: 1

A sharp flat plate of length L and infinite width is immersed parallel to a fluid stream having velocity 𝑢∞. At a point on the plate, far away from the leading edge and not near the trailing edge, the boundary layer thickness, the displacement thickness, and the momentum thickness are denoted as 𝛿, 𝛿∗, and 𝜃, respectively. Which one of the following options correctly represents the relation between these thicknesses?

  • A. 𝛿> 𝛿∗> 𝜃
  • B. 𝛿> 𝜃> 𝛿∗
  • C. 𝛿∗> 𝛿> 𝜃
  • D. 𝜃> 𝛿∗> 𝛿

Answer: A. 𝛿> 𝛿∗> 𝜃

Question 3

Year: 2025 | Marks: 1

Consider the following Statements [1] and [2]. Statement [1]: The Eulerian study focusses attention on individual particle and its motion is observed as a function of time. Statement [2]: The Lagrangian study focusses attention on the motion of the particles passing through an identified point. Which one of the following options identifies the correctness of the given statements?

  • A. Both [1] and [2] are correct.
  • B. Both [1] and [2] are NOT correct.
  • C. [1] is correct, but [2] is NOT correct.
  • D. [1] is NOT correct, but [2] is correct.

Answer: B. Both [1] and [2] are NOT correct.

Question 4

Year: 2025 | Marks: 1

Statement of Reynolds Transport Theorem is given below with three blanks. The rate of change of ________ extensive property can be calculated by summing the rate of change of the amount of same property in the ________ and the rate at which the property is ________ the surface of the control volume. Which one of the following options correctly fills the blanks by using its comma-separated phrases in sequence?

  • A. system, control volume, exiting
  • B. control volume, system, exiting
  • C. system, control volume, entering
  • D. control volume, control volume, entering

Answer: A. system, control volume, exiting

Question 5

Year: 2025 | Marks: 1

For a steady and incompressible flow, the velocity field (𝑉⃗ ) in Cartesian (𝑥, 𝑦, 𝑧) coordinate system is given as: 𝑉⃗ = 5𝑥𝑖−𝑃𝑦𝑗+ 3𝑘 Here, 𝑖, 𝑗, and 𝑘 are unit vectors along x, y, and z directions, respectively and 𝑃 is a constant. Which one of the following options is the correct value of 𝑃 that satisfies the conservation of mass for the given velocity field?

  • A. 5
  • B. −5
  • C. 8
  • D. 2

Answer: A. 5

Question 6

Year: 2025 | Marks: 1

Conservation of mass for a steady axisymmetric flow field in the cylindrical (r, z) coordinates is: 1 𝑟 𝜕(𝑟𝑉𝑟) 𝜕𝑟 + 𝜕𝑉𝑧 𝜕𝑧= 0 Here, 𝑉𝑟 and 𝑉𝑧 are radial and axial components of velocity, respectively. Which one of the following options is correct if 𝜓 is the stream function?

  • A. 𝑉𝑟= 𝜕𝜓 𝜕𝑧 and 𝑉𝑧= − 1 𝑟 𝜕𝜓 𝜕𝑟
  • B. 𝑉𝑟= 1 𝑟 𝜕𝜓 𝜕𝑧 and 𝑉𝑧= − 1 𝑟 𝜕𝜓 𝜕𝑟
  • C. 𝑉𝑟= 1 𝑟 𝜕𝜓 𝜕𝑧 and 𝑉𝑧= 1 𝑟 𝜕𝜓 𝜕𝑟
  • D. 𝑉𝑟= 1 𝑟 𝜕𝜓 𝜕𝑧 and 𝑉𝑧= − 𝜕𝜓 𝜕𝑟

Answer: B. 𝑉𝑟= 1 𝑟 𝜕𝜓 𝜕𝑧 and 𝑉𝑧= − 1 𝑟 𝜕𝜓 𝜕𝑟

Question 7

Year: 2025 | Marks: 1

Group-I indicates different properties of fluid and Group-II defines their basic dimensions in terms of Force (𝐹), Length (𝐿), and Time (𝑇). Group-I Group-II P Dynamic viscosity 1 𝐹𝐿−4𝑇2 Q Surface tension 2 𝐹𝐿−2𝑇 R Density 3 𝐹𝐿−1 Which one of the following options identifies the correct match between Group-I and Group-II?

  • A. P−1, Q−3, R−2
  • B. P−2, Q−1, R−3
  • C. P−3, Q−2, R−1
  • D. P−2, Q−3, R−1

Answer: D. P−2, Q−3, R−1

Question 8

Year: 2025 | Marks: 1

Consider the steady, incompressible, and fully developed laminar flow of a fluid through a circular pipe. Here, ∆𝑃 is the pressure drop in the direction of the flow and 𝑉 is the average axial velocity of the fluid at any cross-section. The relation between ∆𝑃 and 𝑉 is: ∆𝑃= 𝐾 𝑉𝑛 Here, 𝐾 and 𝑛 are constants. Which one of the following options is the correct value of 𝑛?

  • A. 1
  • B. 2
  • C. 1.75
  • D. 0.5

Answer: A. 1

Question 9

Year: 2025 | Marks: 1

A doublet is the resulting flow pattern when a sink and a source of equal strength are brought together. Which one of the following options correctly represents the nature of the product of the strength and the distance between them during approach?

  • A. Remains always constant
  • B. Continuously decreases
  • C. Continuously increases
  • D. First increases and then continuously decreases after reaching a maximum

Answer: A. Remains always constant

Question 10

Year: 2025 | Marks: 2

Figure shows two parallel plates (upper plate at 𝑥= 𝑏 and lower one at 𝑥= −𝑏) of length L (aligned in 𝑧 direction) and infinite width (in 𝑦 direction, normal to the plane of the figure). Two immiscible, incompressible liquids are flowing steadily in the 𝑧 direction through the thin passage between the plates under the influence of horizontal pressure gradient (𝑃0 −𝑃𝐿) L ⁄ . During the flow, the passage is always half-filled with denser fluid I (viscosity 𝜇𝐼) at the bottom and rest is occupied by lighter fluid II (viscosity 𝜇𝐼𝐼; 𝜇𝐼𝐼< 𝜇𝐼). Considering exactly planar interface between the fluids and no instabilities in the flow, the shear stress, 𝜏𝑥𝑧 is expressed as: 𝜏𝑥𝑧= (𝑃0 −𝑃𝐿)𝑏 L [(𝑥 𝑏) −1 2 (𝜇𝐼−𝜇𝐼𝐼 𝜇𝐼+ 𝜇𝐼𝐼)] Which one of the following options correctly identifies the location of the point having maximum velocity of the flow?

Figure for question 10, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. Above the interface
  • B. Below the interface
  • C. At the interface
  • D. At the top plate

Answer: A. Above the interface

Question 11

Year: 2025 | Marks: 2

Group-I shows different two-dimensional bodies and Group-II mentions their total drag coefficient (𝐶𝐷) based on frontal area while facing parallel flow of fluid having Reynolds number 𝑅𝑒≥104 along the direction of arrow. The bodies are placed symmetrically with respect to the flow direction. Group-I Group-II P 1 1.2 Q 2 1.6 R 3 2.1 S 4 2.3 Which one of the following options identifies the correct match between Group-I and Group-II, as per the concept of degree of streamlining?

Figure for question 11, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. P−3, Q−2, R−1, S−4
  • B. P−3, Q−2, R−4, S−1
  • C. P−2, Q−3, R−1, S−4
  • D. P−3, Q−1, R−2, S−4

Answer: A. P−3, Q−2, R−1, S−4

Question 12

Year: 2025 | Marks: 2

A solid body of uniform specific gravity floats in a deep liquid pool. Take 𝐵, 𝐺, and 𝑀 as the centre of buoyancy, centre of gravity, and metacentre of the body, respectively. Which one of the following options is correct for the stable floatation of the body in the pool when the body is given a small tilt angle?

  • A. 𝑀𝐺̅̅̅̅̅ is the metacentric height and 𝐺 should lie below 𝑀
  • B. 𝑀𝐺̅̅̅̅̅ is the metacentric height and 𝐵 should lie above 𝑀
  • C. 𝑀𝐵̅̅̅̅̅ is the metacentric height and 𝐵 should lie below 𝑀
  • D. 𝑀𝐵̅̅̅̅̅ is the metacentric height and 𝐺 should lie above 𝑀

Answer: A. 𝑀𝐺̅̅̅̅̅ is the metacentric height and 𝐺 should lie below 𝑀

Question 13

Year: 2025 | Marks: 2

Figure shows the steady and incompressible flow of a fluid in the direction of arrow from section A to section D. Three pipe connectors are to be placed between sections at A and D having Total Energy Line (TEL) and Hydraulic Grade Line (HGL) as depicted in the figure. Consider, g, P, Q, V, γ, and Z denote gravitational acceleration, pressure, volume flow rate, velocity, specific weight, and elevation of centerline of the pipe connectors from the datum, respectively. Which one of the following options, in sequence, indicates the correct nature of connectors between sections A and B, B and C, and C and D in the direction of flow?

Figure for question 13, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. Converging, Constant area, Diverging
  • B. Diverging, Constant area, Converging
  • C. Constant area, Constant area, Constant area
  • D. Constant area, Converging, Diverging

Answer: A. Converging, Constant area, Diverging

Question 14

Year: 2025 | Marks: 2

A liquid flows under steady and incompressible flow conditions from station 1 to station 4 through pipe sections P, Q, R, and S as shown in figure. Consider, 𝑑, 𝑉, and ℎ represent the diameter, velocity, and head loss, respectively, in each pipe section with subscripts ‘P’, ‘Q’, ‘R’, and ‘S’. ∆ℎ represents the head difference between the inlet (station 1) and outlet (station 4). All the pipe sections are placed on the same horizontal plane for which the figure shows the top view. Which one of the following options is correct for the given flow loop?

Figure for question 14, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ∆ℎ= ℎ𝑃+ ℎ𝑄+ ℎ𝑅+ ℎ𝑆 and 𝑉𝑃𝑑𝑃 2 = 𝑉𝑄𝑑𝑄 2 = 𝑉𝑅𝑑𝑅 2 = 𝑉𝑆𝑑𝑆 2
  • B. ∆ℎ= ℎ𝑃+ ℎ𝑄+ ℎ𝑅 and 𝑉𝑃𝑑𝑃 2 = 𝑉𝑄𝑑𝑄 2 = 𝑉𝑅𝑑𝑅 2 = 𝑉𝑆𝑑𝑆 2
  • C. ∆ℎ= ℎ𝑃+ ℎ𝑄+ ℎ𝑅 and 𝑉𝑃𝑑𝑃 2 = 𝑉𝑄𝑑𝑄 2 = 𝑉𝑅𝑑𝑅 2 + 𝑉𝑆𝑑𝑆 2
  • D. ∆ℎ= ℎ𝑃+ ℎ𝑄+ ℎ𝑅+ ℎ𝑆 and 𝑉𝑃𝑑𝑃 2 = 𝑉𝑄𝑑𝑄 2 = 𝑉𝑅𝑑𝑅 2 + 𝑉𝑆𝑑𝑆 2

Answer: C. ∆ℎ= ℎ𝑃+ ℎ𝑄+ ℎ𝑅 and 𝑉𝑃𝑑𝑃 2 = 𝑉𝑄𝑑𝑄 2 = 𝑉𝑅𝑑𝑅 2 + 𝑉𝑆𝑑𝑆 2

Question 15

Year: 2025 | Type: NAT | Marks: 2

Consider, 𝑖 and 𝑗 are unit vectors along x and y directions of a Cartesian (𝑥, 𝑦) coordinate system, respectively and 𝑡 is time. Temperature (𝑇) and fluid velocity (𝑉⃗ ) are given for a flow field as: 𝑇= 𝑥2 + 𝑦𝑡+ 35 𝑉⃗ = (4𝑥𝑦)𝑖+ (𝑥𝑡−2𝑦2)𝑗 The total rate of change of temperature in the flow field (in integer) for time 𝑡= 2 at a point (2, 3) is ________

Answer: 71

Question 16

Year: 2025 | Type: NAT | Marks: 2

Driven by a pressure gradient of 100 kPa/m, a fluid of dynamic viscosity 0.1 Pa.s flows between two fixed infinitely large parallel plates under steady, incompressible, and fully developed laminar conditions. The average velocity of the flow is 2 m/s. The gap between the parallel plates in mm (rounded off to 2 decimal places) is ________

Answer: 4.80 to 5.00

Question 17

Year: 2025 | Type: NAT | Marks: 2

An incompressible fluid is flowing between two infinitely large parallel plates separated by 5 mm distance. The bottom plate is stationary and the top plate is moving at a constant velocity of 5 mm/s in the direction parallel to the bottom plate. The flow of the fluid between the plates is steady, two-dimensional, laminar, and the variation of fluid velocity is linear between the plates. A square fluid element of 1 mm side is considered at equal distance from both the plates in the flow field such that one of its sides is parallel to the plates. The magnitude of circulation in mm2/s (in integer) along the edges of the square fluid element is ________

Answer: 1

Question 18

Year: 2025 | Type: NAT | Marks: 2

Consider, a kite weighing 100 grams as essentially a rigid flat plate making an angle 8° with the horizontal and having a planform area of 0.045 m2 when exposed to horizontal parallel wind of 60 km/h. The thread string of the kite makes an angle 45° with the horizontal. A tension of 450 grams in the thread is necessary to float the kite steadily. Take air density as 1.2 kg/m3 and gravitational acceleration as 9.81 m/s2. The lift coefficient (𝐶𝐿) associated with the air flow around steadily floating kite (rounded off to 2 decimal places) is ________

Answer: 0.50 to 0.60

Question 19

Year: 2025 | Type: NAT | Marks: 2

A fixed control volume has four one-dimensional boundary sections (1, 2, 3, and 4). For a steady flow inside the control volume, the flow properties at each section are tabulated below: Boundary Section Type Density (kg/m3) Surface Normal Velocity (m/s) Cross-sectional Area (m2) Specific Energy (J/kg) 1 Inlet 1000 10 0.5 200 2 Inlet 1000 2 3.0 50 3 Outlet 1000 5 1.0 100 4 Outlet 1000 4 1.5 80 The rate of change of energy of the system which occupies the control volume at this instant is 𝐸× 106 J/s. The value of 𝐸 (rounded off to 2 decimal places) is ________

Answer: -0.32

Question 20

Year: 2025 | Type: NAT | Marks: 2

A ship is to be operated in a fluid medium with kinematic viscosity 0.032 × 10−3 m2/s. A one-tenth scale model of the ship is built for testing. Consider, inertia, viscous and gravity forces are dominant for the ship and its model during the operation. The required kinematic viscosity of the liquid for testing the model is 𝑃× 10−6 m2/s. The value of 𝑃 (rounded off to 2 decimal places) is ________

Answer: 0.95 to 1.05

Question 21

Year: 2025 | Type: NAT | Marks: 2

Water flows through a pipe of diameter 20 cm at a flow rate of 0.025 m3/s. A pitot- static tube is placed at the centre of the pipe and indicates the pressure difference of 5 cm of water column. Theoretical velocity measured through pitot-static tube when multiplied with velocity coefficient 𝐶𝑉 gives the actual velocity of the flow. If the mean velocity in the pipe is 90% of the actual velocity at the centre of the pipe and the gravitational acceleration is 10 m/s2, the value of 𝐶𝑉 (rounded off to 2 decimal places) is ________

Answer: 0.85 to 0.90

Question 22

Year: 2025 | Type: NAT | Marks: 2

An oil of density 870 kg/m3 and viscosity 0.036 Pa.s flows through a straight pipe of 10 cm diameter and 1.5 km length at the flow rate of 250 liters per minute under the steady and incompressible flow conditions. To control the flow rate of oil, a valve is fixed at the middle of the pipe causing no change in the total length of the pipe. The total head loss measured across the two ends of the pipe is 11.60 m. Using gravitational acceleration as 10 m/s2, the minor head loss contributed by the presence of the valve in m (rounded off to 2 decimal places) is ________

Answer: 0.85 to 1.28

Question 23

Year: 2024 | Marks: 1

Which one of the following figures shows the CORRECT dependence of apparent viscosity (η) on rate of shear strain (𝑑𝑢/𝑑𝑦) for pseudoplastic fluids?

Figure for question 23, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 24

Year: 2024 | Marks: 1

The locus of temporary locations of all particles that have passed through a fixed point in the flow field at a particular instant is known as

  • A. streamline.
  • B. streakline.
  • C. pathline.
  • D. timeline.

Answer: B. streakline.

Question 25

Year: 2024 | Marks: 1

Consider the velocities 𝑢, 𝑣, and 𝑤 in x-, y-, and z-directions, respectively. The vorticity expression in the y-z plane is

  • A. 𝜕𝑣 𝜕𝑥−𝜕𝑢 𝜕𝑦
  • B. 𝜕𝑣 𝜕𝑦−𝜕𝑤 𝜕𝑧
  • C. 𝜕𝑤 𝜕𝑦−𝜕𝑣 𝜕𝑧
  • D. 𝜕𝑢 𝜕𝑧−𝜕𝑤 𝜕𝑥

Answer: C. 𝜕𝑤 𝜕𝑦−𝜕𝑣 𝜕𝑧

Question 26

Year: 2024 | Marks: 1

For the laminar, incompressible flow over a flat plate with uniform free stream velocity, the axial pressure gradient within the boundary layer is

  • A. greater than zero.
  • B. less than zero.
  • C. equal to zero.
  • D. equal to the axial velocity gradient.

Answer: C. equal to zero.

Question 27

Year: 2024 | Marks: 1

Let 𝑟 , 𝑉⃗ , and 𝑚 be position vector, velocity vector, and mass, respectively in a control mass system. Which one of the following properties is considered as conserved extensive property in Reynolds Transport Theorem to obtain the angular momentum equation?

  • A. 𝑟 × 𝑚𝑉⃗
  • B. 𝑟 × 𝑉⃗
  • C. 𝑚𝑉⃗
  • D. 𝑚

Answer: A. 𝑟 × 𝑚𝑉⃗

Question 28

Year: 2024 | Marks: 1

The hydraulic diameter for a circular pipe of radius 𝑅 is

  • A. 0.5R
  • B. R
  • C. 2R
  • D. 4R

Answer: C. 2R

Question 29

Year: 2024 | Marks: 1

For incompressible, laminar, fully-developed flow through a circular pipe, Darcy friction factor and Fanning friction factor are represented as 𝑓 and 𝐶𝑓, respectively. Which one of the following options is correct?

  • A. 𝑓= 0.25𝐶𝑓
  • B. 𝑓= 0.5𝐶𝑓
  • C. 𝑓= 2𝐶𝑓
  • D. 𝑓= 4𝐶𝑓

Answer: D. 𝑓= 4𝐶𝑓

Question 30

Year: 2024 | Marks: 1

For an immersed neutrally buoyant body to be in stable equilibrium, the center of gravity of the body is directly

  • A. above the metacenter.
  • B. below the metacenter.
  • C. above the center of buoyancy.
  • D. below the center of buoyancy.

Answer: D. below the center of buoyancy.

Question 31

Year: 2024 | Type: NAT | Marks: 1

The absolute pressure in a chamber is measured as 400 mm Hg at a location where the atmospheric pressure is 700 mm Hg. A vacuum gauge connected to the chamber reads ________ mm Hg (answer in integer).

Answer: 300

Question 32

Year: 2024 | Marks: 2

A thin film of an incompressible, Newtonian liquid (density 𝜌,⁡viscosity 𝜇) with an uniform thickness (h) is flowing down on a vertical plate. The flow is driven by gravity (𝑔) alone. Assume zero shear stress condition at the free surface. The maximum velocity is given by

Figure for question 32, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1 2𝜇𝜌𝑔ℎ2
  • B. 1 4𝜇𝜌𝑔ℎ2
  • C. 1 𝜇𝜌𝑔ℎ2
  • D. 1 8𝜇𝜌𝑔ℎ2

Answer: A. 1 2𝜇𝜌𝑔ℎ2

Question 33

Year: 2024 | Marks: 2

A one-eighth scale model of a car is to be tested in a wind tunnel. If the air velocity over the car is 16 m/s, what should be the air velocity (in m/s) in the wind tunnel in order to achieve similarity between the model and the prototype?

  • A. 2
  • B. 16
  • C. 64
  • D. 128

Answer: D. 128

Question 34

Year: 2024 | Marks: 2

A set of basic dimensions, mass, length, and time are represented by M, L, and T, respectively. What will be the dimensions of pressure in M-L-T system?

  • A. ML−1T −2
  • B. MLT −2
  • C. MLT −1
  • D. ML−1T −1

Answer: A. ML−1T −2

Question 35

Year: 2024 | Marks: 2

Consider a fluid flow around an airfoil as shown in figure. The directions of drag force and lift force, respectively are along

Figure for question 35, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. OA and OC.
  • B. OA and OD.
  • C. OB and OC.
  • D. OB and OD.

Answer: D. OB and OD.

Question 36

Year: 2024 | Type: NAT | Marks: 2

A vessel which contains a volatile liquid and its vapour is connected with a mercury manometer as shown in figure. Both the liquid and vapour phases are at equilibrium. The vapour pressure and density of the volatile liquid are 107.6 kPa and 700 kg/m3, respectively. The density of the mercury is 13600 kg/m3. Acceleration due to gravity (g) is 10 m/s2 and atmospheric pressure is 101 kPa. Hydrostatic pressure created by the weight of the vapour is neglected. The height, h (in m, rounded off to two decimal places) of the mercury column in figure is _________.

Figure for question 36, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.09 to 0.11

Question 37

Year: 2024 | Type: NAT | Marks: 2

The velocity in a one-dimensional flow is given by 𝑢(𝑥) = 𝑎 (𝑏−𝑥)2 m/s, where 𝑎= 8 m3/s and 𝑏= 4 m. The acceleration (in m/s2, answer in integer) at 𝑥= 2 m is _____.

Answer: 4

Question 38

Year: 2024 | Type: NAT | Marks: 2

Consider two parallel plates separated by a distance of 1 cm filled with a Newtonian fluid of viscosity 10-3 Pa.s. The top plate is moving with a velocity of 1 m/s whereas the bottom plate is stationary. The shear stress (in Pa, rounded off to one decimal place) on the top plate is _____ .

Answer: 0.1

Question 39

Year: 2024 | Type: NAT | Marks: 2

A circular water jet of diameter 50 mm impinges with a velocity of 18 m/s normal to a plate. The density of water is 1000 kg/m3 and gravity force is neglected. The magnitude of net force (in N, rounded off to two decimal places) imparted by the jet on the stationary plate is _______________.

Figure for question 39, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 635.00 to 637.00

Question 40

Year: 2024 | Type: NAT | Marks: 2

Consider the steady, incompressible flow of water in a horizontal pipe of constant diameter 1 m with an inlet velocity of 12 m/s. As shown in figure, water is lost through a circular hole of diameter 0.6 m at the rate of 4.53 m3/s. The outlet velocity (in m/s, rounded off to two decimal places) of water in the pipe is ______.

Figure for question 40, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 6.00 to 6.50

Question 41

Year: 2024 | Type: NAT | Marks: 2

The axial velocity profile of a laminar, incompressible and fully-developed flow in a circular pipe of radius (R) is given as 𝑢𝑧= − 1 4𝜇 𝜕𝑝 𝜕𝑧𝑅2 (1 − 𝑟2 𝑅2), where r, 𝑧, 𝜇, and 𝑝 are radial direction, axial direction, fluid viscosity, and pressure, respectively. If the average velocity of the flow is given by 𝑢𝑧,𝑎𝑣𝑔= 1 𝐾(− 𝑅2 𝜇 𝜕𝑝 𝜕𝑧), then the value of K (answer in integer) is ______.

Answer: 8

Question 42

Year: 2024 | Type: NAT | Marks: 2

The velocity potential function in a two-dimensional flow field is given by 𝜙(𝑥, 𝑦) = −(𝑎𝑥𝑦+ 𝑏𝑥2 −𝑏𝑦2) m2/s where a = 2 per second and b = 0.5 per second. The magnitude of the velocity (in m/s, answer in integer) at 𝑥= 2 m, 𝑦= 1 m is _____.

Answer: 5

Question 43

Year: 2024 | Type: NAT | Marks: 2

Consider the incompressible, steady and irrotational flow through a concentric reducer in a horizontal pipeline. The pipe diameter reduces from d1 = 12 cm to d2 = 4 cm as shown in figure. The pressure at position 1 and position 2 of the reducer is p1 = 55 kPa and p2 = 27 kPa, respectively. The specific weight of fluid is 7 kN/m3. Acceleration due to gravity is 10 m/s2. Neglecting frictional effects, the mass flow rate (in kg/s, rounded off to two decimal places) of the fluid through the reducer is _____.

Figure for question 43, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 7.85 to 8.11

Question 44

Year: 2024 | Type: NAT | Marks: 2

Consider the incompressible fluid flow over a flat plate with a free stream velocity, 𝑈∞= 1 m/s. The fluid kinematic viscosity is 10−6 m2/s and density is 1 kg/m3. The velocity profile within the boundary layer at any location 𝑥 is given by 𝑢(𝑦) = 𝑈∞( 3 2 𝑦 𝛿− 1 2 𝑦2 𝛿2), where boundary layer thickness, 𝛿= 4.64𝑥 √𝑅𝑒𝑥. The local wall shear stress at 𝑥= 1 m from the leading edge is _____ × 10 -3 N/m2 (rounded off to two decimal places).

Answer: 0.30 to 0.35

Question 45

Year: 2023 | Marks: 1

Match the following measuring instruments with the appropriate figures. I – Pitot probe II – Pitot-static probe III – Piezometer

Figure for question 45, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. I – P; II – Q; III – R
  • B. I – R; II – Q; III – P
  • C. I – R; II – P; III – Q
  • D. I – Q; II – P; III – R

Answer: B. I – R; II – Q; III – P

Question 46

Year: 2023 | Marks: 1

Among the following non-dimensional numbers, which one characterizes periodicity present in a transient flow?

  • A. Froude number
  • B. Strouhal number
  • C. Peclet number
  • D. Lewis number

Answer: B. Strouhal number

Question 47

Year: 2023 | Marks: 1

For an incompressible boundary layer flow over a flat plate shown in the figure, the momentum thickness is expressed as

Figure for question 47, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ∫ 𝑢 𝑈∞ 𝑑𝑦 ∞ 0
  • B. ∫ (1 −𝑢 𝑈∞ ) 𝑑𝑦 ∞ 0
  • C. ∫ 𝑢 𝑈∞ (1 −𝑢 𝑈∞ ) 𝑑𝑦 ∞ 0
  • D. ∫ (1 −𝑢2 𝑈∞2 ) 𝑑𝑦 ∞ 0

Answer: C. ∫ 𝑢 𝑈∞ (1 −𝑢 𝑈∞ ) 𝑑𝑦 ∞ 0

Question 48

Year: 2023 | Marks: 1

Among the shear stress versus shear strain rate curves shown in the figure, which one corresponds to a shear thinning fluid?

Figure for question 48, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. P
  • B. Q
  • C. R
  • D. S

Answer: C. R

Question 49

Year: 2023 | Marks: 1

Consider steady incompressible flow over a flat plate, where the dashed line represents the edge of the boundary layer, as shown in the figure. Which one among the following statements is true?

Figure for question 49, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. Bernoulli’s equation can be applied in Region I between any two arbitrary points.
  • B. Bernoulli’s equation can be applied in Region I only along a streamline.
  • C. Bernoulli’s equation cannot be applied in Region II.
  • D. Bernoulli’s equation cannot be applied in Region I.

Answer: D. Bernoulli’s equation cannot be applied in Region I.

Question 50

Year: 2023 | Marks: 1

An inviscid steady incompressible flow is formed by combining a uniform flow with velocity 𝑈∞ and a clockwise vortex of strength 𝐾 at the origin, as shown in the figure. Velocity potential (𝜙) for the combined flow in polar coordinate (𝑟, 𝜃) is

Figure for question 50, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 𝜙= 𝐾𝜃 2 𝜋−𝑈∞𝑟 cos 𝜃
  • B. 𝜙= 𝐾𝜃 2 𝜋−𝑈∞𝑟 sin 𝜃
  • C. 𝜙= 𝐾ln 𝑟+ 𝑈∞𝑟 cos 𝜃
  • D. 𝜙= −𝐾ln 𝑟+ 𝑈∞𝑟 sin 𝜃

Answer: A. 𝜙= 𝐾𝜃 2 𝜋−𝑈∞𝑟 cos 𝜃

Question 51

Year: 2023 | Marks: 1

Which of the following statements are true? (i) Conservation of mass for an unsteady incompressible flow can be represented as ∇⋅𝑉⃗⃗= 0, where 𝑉⃗⃗ denotes velocity vector. (ii) Circulation is defined as the line integral of vorticity about a closed curve. (iii) For some fluids, shear stress can be a nonlinear function of the shear strain rate. (iv) Integration of the Bernoulli’s equation along a streamline under steady-state leads to the Euler’s equation.

  • A. (i), (ii) and (iv) only
  • B. (i), (ii) and (iii) only
  • C. (i) and (iii) only
  • D. (ii) and (iv) only

Answer: C. (i) and (iii) only

Question 52

Year: 2023 | Marks: 1

For a two-dimensional flow field given as 𝑉⃗⃗= −𝑥𝑖̂ + 𝑦𝑗̂, a streamline passes through points (2, 1) and (5, p). The value of p is

  • A. 5
  • B. 5/2
  • C. 2/5
  • D. 2

Answer: C. 2/5

Question 53

Year: 2023 | Type: MSQ | Marks: 1

A stationary object is fully submerged in a static fluid, as shown in the figure. Here, CG and CB stand for center of gravity and center of buoyancy, respectively. Which one(s) among the following statements is/are true?

Figure for question 53, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. The object is in stable equilibrium if 𝑦𝐶𝐺> 𝑦𝐶𝐵.
  • B. The object is in stable equilibrium if 𝑦𝐶𝐺< 𝑦𝐶𝐵.
  • C. The object is in neutral equilibrium if 𝑦𝐶𝐺= 𝑦𝐶𝐵.
  • D. The object is in unstable equilibrium if 𝑦𝐶𝐺= 𝑦𝐶𝐵.

Answer: A. The object is in stable equilibrium if 𝑦𝐶𝐺> 𝑦𝐶𝐵.; C. The object is in neutral equilibrium if 𝑦𝐶𝐺= 𝑦𝐶𝐵.

Question 54

Year: 2023 | Marks: 2

Consider steady fully-developed incompressible flow of a Newtonian fluid between two infinite parallel flat plates. The plates move in the opposite directions, as shown in the figure. In the absence of body force and pressure gradient, the ratio of shear stress at the top surface (𝑦= 𝐻) to that at the bottom surface (𝑦= 0) is

Figure for question 54, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1
  • B. 𝑈1 𝑈2
  • C. 𝑈1 −𝑈2 𝑈2
  • D. 𝑈1 + 𝑈2 𝑈2

Answer: A. 1

Question 55

Year: 2023 | Marks: 2

A two-dimensional incompressible flow field is defined as, 𝑉⃗⃗(𝑥, 𝑦) = (𝐴𝑥𝑦) 𝑖̂ + (𝐵𝑦2) 𝑗̂ where, 𝐴 and 𝐵 are constants. The dynamic viscosity of the Newtonian fluid is 𝜇. In the absence of body force, which among the following expressions represents the pressure gradient at the location (5, 0) in the concerned flow field?

  • A. 𝜇𝐴(5 𝑖̂ + 𝑗̂)
  • B. 𝜇(−5𝐵 𝑖̂ + 𝐴 𝑗̂)
  • C. 𝜇𝐴(−𝑗̂)
  • D. 𝜇𝐴(5 𝑖̂)

Answer: C. 𝜇𝐴(−𝑗̂)

Question 56

Year: 2023 | Marks: 2

For a potential flow, the fluid velocity is given by 𝑉⃗⃗(𝑥, 𝑦) = 𝑢𝑖̂ + 𝑣𝑗̂ . The slope of the potential line at (𝑥, 𝑦) is

  • A. 𝑢 𝑣
  • B. 𝑣 𝑢
  • C. −𝑢 𝑣
  • D. −𝑣 𝑢

Answer: C. −𝑢 𝑣

Question 57

Year: 2023 | Marks: 2

Consider steady incompressible flow of a Newtonian fluid over a horizontal flat plate, as shown in the figure. The boundary layer thickness is proportional to

Figure for question 57, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 𝑥1/4
  • B. 𝑥1/2
  • C. 𝑥−1/2
  • D. 𝑥2

Answer: B. 𝑥1/2

Question 58

Year: 2023 | Type: MSQ | Marks: 2

In a steady two-dimensional compressible flow, 𝑢 and 𝑣 are the 𝑥- and 𝑦- components of flow velocity, respectively and 𝜌 is the fluid density. Among the following pairs of relations, which one(s) perfectly satisfies/satisfy the definition of stream function, 𝜓, for this flow?

  • A. 𝑢= 𝜕𝜓 𝜕𝑦 and 𝑣= − 𝜕𝜓 𝜕𝑥
  • B. 𝑢= − 𝜕𝜓 𝜕𝑥 and 𝑣= − 𝜕𝜓 𝜕𝑦
  • C. 𝜌𝑢= 𝜕𝜓 𝜕𝑦 and 𝜌𝑣= − 𝜕𝜓 𝜕𝑥
  • D. 𝜌𝑢= − 𝜕𝜓 𝜕𝑦 and 𝜌𝑣= 𝜕𝜓 𝜕𝑥

Answer: C. 𝜌𝑢= 𝜕𝜓 𝜕𝑦 and 𝜌𝑣= − 𝜕𝜓 𝜕𝑥; D. 𝜌𝑢= − 𝜕𝜓 𝜕𝑦 and 𝜌𝑣= 𝜕𝜓 𝜕𝑥

Question 59

Year: 2023 | Type: NAT | Marks: 2

A water jet (density = 1000 kg/m3) is approaching a vertical plate, having an orifice at the center, as shown in the figure. While a part of the jet passes through the orifice, remainder flows along the plate. Neglect friction and assume both the inlet and exit jets to have circular cross-sections. If V = 5 m/s, 𝐷 = 100 mm and 𝑑 = 25 mm, magnitude of the horizontal force (in N, rounded off to one decimal place) required to hold the plate in its position is ___________.

Figure for question 59, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 183.0 to 185.0

Question 60

Year: 2023 | Type: NAT | Marks: 2

Water (density = 1000 kg/m3) and alcohol (specific gravity = 0.7) enter a Y-shaped channel at flow rates of 0.2 m3/s and 0.3 m3/s, respectively. Their mixture leaves through the other end of the channel, as shown in the figure. The average density (in kg/m3) of the mixture is _______.

Figure for question 60, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 820

Question 61

Year: 2023 | Type: NAT | Marks: 2

The velocity and acceleration of a fluid particle are given as 𝑉⃗⃗= (−𝑖̂ + 2𝑗̂) m/s and 𝑎⃗= (−2𝑖̂ −4𝑗̂) m/s2, respectively. The magnitude of the component of acceleration (in m/s2, rounded off to two decimal places) of the fluid particle along the streamline is _______.

Answer: 2.60 to 2.75

Question 62

Year: 2023 | Type: NAT | Marks: 2

A hydraulic turbine with rotor diameter of 100 mm produces 200 W of power while rotating at 300 rpm. Another dynamically-similar turbine rotates at a speed of 1500 rpm. Consider both turbines to operate with the same fluid (identical density and viscosity), and neglect any gravitational effect. Then the power (in W, rounded off to nearest integer) produced by the second turbine is _______________.

Answer: 430 to 460

Question 63

Year: 2023 | Type: NAT | Marks: 2

Water (density = 1000 kg/m3) flows steadily with a flow rate of 0.05 m3/s through a venturimeter having throat diameter of 100 mm. If the pipe diameter is 200 mm and losses are negligible, the pressure drop (in kPa, rounded off to one decimal place) between an upstream location in the pipe and the throat (both at the same elevation) is _______.

Answer: 18.5 to 19.5

Question 64

Year: 2023 | Type: NAT | Marks: 2

Water flows around a thin flat plate (0.25 m long, 2 m wide) with a free stream velocity (𝑈∞) of 1 m/s, as shown in the figure. Consider linear velocity profile ( 𝑢 𝑈∞= 𝑦 𝛿) for which the laminar boundary layer thickness is expressed as 𝛿= 3.5𝑥 √𝑅𝑒𝑥 . For water, density = 1000 kg/m3 and dynamic viscosity = 0.001 kg/m.s. Net drag force (in N, rounded off to two decimal places) acting on the plate, neglecting the end effects, is ________.

Figure for question 64, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 1.10 to 1.20

Question 65

Year: 2023 | Type: NAT | Marks: 2

Axial velocity profile 𝑢(𝑟) for an axisymmetric flow through a circular tube of radius 𝑅 is given as, 𝑢(𝑟) 𝑈 = (1 −𝑟 𝑅) 1 𝑛 ⁄ where 𝑈 is the centerline velocity. If 𝑉 refers to the area-averaged velocity (volume flow rate per unit area), then the ratio 𝑉/𝑈 for 𝑛= 1 (rounded off to two decimal places) is ______________.

Answer: 0.32 to 0.34

Question 66

Year: 2023 | Type: NAT | Marks: 2

A stationary circular pipe of radius 𝑅= 0.5 m is half filled with water (density = 1000 kg/m3), whereas the upper half is filled with air at atmospheric pressure, as shown in the figure. Acceleration due to gravity is 𝑔= 9.81 m/s2. The magnitude of the force per unit length (in kN/m, rounded off to one decimal place) applied by water on the pipe section AB is _______. Material Science (XE-C)

Figure for question 66, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 2.2 to 2.4

Question 67

Year: 2022 | Marks: 1

A heavy horizontal cylinder of diameter D supports a mass of liquid having density 𝜌 as shown in the figure. Find out the vertical component of force exerted by the liquid per unit length of the cylinder if g is the acceleration due to gravity.

Figure for question 67, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 𝜋𝐷ଶ 4 𝜌𝑔
  • B. 𝜋𝐷ଶ 8 𝜌𝑔
  • C. 𝜋𝐷ଶ 2 𝜌𝑔
  • D. 𝜋𝐷ଶ 3 𝜌𝑔

Answer: B. 𝜋𝐷ଶ 8 𝜌𝑔

Question 68

Year: 2022 | Marks: 1

The figure shows the developing zone and the fully developed region in a pipe flow where the steady flow takes place from left to right. The wall shear stress in the sections A, B, C, and D are given by 𝜏஺, 𝜏஻, 𝜏஼, and 𝜏஽, respectively. Select the correct statement.

Figure for question 68, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 𝜏஺൐ 𝜏஻
  • B. 𝜏஻൐ 𝜏஺
  • C. 𝜏஼൐ 𝜏஻
  • D. 𝜏஼൐ 𝜏஽

Answer: A. 𝜏஺൐ 𝜏஻

Question 69

Year: 2022 | Marks: 1

The left hand column lists some non-dimensional numbers and the right hand column lists some physical phenomena. Indicate the correct combination 1. Reynolds number i. Wave drag 2. Froude number ii. Compressible flow 3. Mach number iii. Viscous drag 4. Weber number iv. Spray formation

  • A. 1-iii, 2-i, 3-ii, 4-iv
  • B. 1-i, 2-ii, 3-iv, 4-iii
  • C. 1-iv, 2-iii, 3-iv, 4-iii
  • D. 2-iv, 1-iii, 3-ii, 4-i

Answer: A. 1-iii, 2-i, 3-ii, 4-iv

Question 70

Year: 2022 | Type: MSQ | Marks: 1

As temperature increases

  • A. the dynamic viscosity of a gas increases.
  • B. the dynamic viscosity of a liquid decreases.
  • C. the dynamic viscosity of a liquid does not change.
  • D. the dynamic viscosity of a gas decreases.

Answer: A. the dynamic viscosity of a gas increases.; B. the dynamic viscosity of a liquid decreases.

Question 71

Year: 2022 | Type: MSQ | Marks: 1

Which of the following statement(s) regarding a venturimeter is/are correct?

  • A. In the direction of flow, it consists of a converging section, a throat, and a diverging section.
  • B. In the direction of flow, it consists of a diverging section, a throat, and a converging section.
  • C. It is used for flow measurement at a very low Reynolds number.
  • D. Pressure tappings are provided just upstream of the venturimeter and at the throat.

Answer: A. In the direction of flow, it consists of a converging section, a throat, and a diverging section.; D. Pressure tappings are provided just upstream of the venturimeter and at the throat.

Question 72

Year: 2022 | Type: MSQ | Marks: 1

Which of the following statement(s) is/are true for streamlines in a steady incompressible flow?

  • A. Two streamlines cannot intersect each other.
  • B. Flow rate increases between two diverging streamlines.
  • C. Flow rate decreases between two diverging streamlines.
  • D. Stream function has a constant value along a streamline.

Answer: A. Two streamlines cannot intersect each other.; D. Stream function has a constant value along a streamline.

Question 73

Year: 2022 | Type: MSQ | Marks: 1

A flow has a velocity potential given by 𝜙ൌ𝐴𝑥ଷ where ‘A’ is a non-zero constant. Which of the following statement(s) is/are true about the flow?

  • A. The flow is incompressible.
  • B. The flow is irrotational.
  • C. The flow has local acceleration.
  • D. The flow has convective acceleration.

Answer: B. The flow is irrotational.; D. The flow has convective acceleration.

Question 74

Year: 2022 | Type: MSQ | Marks: 1

A boundary layer develops due to a two-dimensional steady flow over a horizontal flat plate. Consider a vertical line away from the leading edge which extends from the wall to the edge of the boundary layer. Which of the following quantity/quantities is/are not constant along the vertical line? 𝑢 and 𝑣 represent the components of velocity in the direction along the plate and normal to it, respectively and x is taken along the length of the plate while p is the pressure. Neglect body forces.

  • A. 𝑢
  • B. 𝜕𝑢 𝜕𝑥
  • C. 𝑣
  • D. 𝑝

Answer: A. 𝑢; B. 𝜕𝑢 𝜕𝑥; C. 𝑣

Question 75

Year: 2022 | Type: NAT | Marks: 1

A 10 kg mass placed on an infinitely long horizontal massless flat platform is to be supported by a steady vertical water jet as shown in the figure. The diameter of the jet is 5 cm. What minimum average velocity is required to hold the mass in place? Assume 𝜌௪௔௧௘௥ൌ1000 kg/mଷ, 𝑔ൌ10 ୫ ୱమ and 𝜋ൌ3.14 . Neglect friction. (Round off to two decimal places)

Figure for question 75, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 6.95 to 7.20

Question 76

Year: 2022 | Marks: 2

Consider an inviscid flow through a smooth pipe which has a pitot-static tube arrangement as shown. Find the centre-line velocity in the pipe. Consider that the density of the fluid is 1000 kg/m3, acceleration due to gravity is 10 m/s2, and the specific gravity of the manometric fluid is 11.

Figure for question 76, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 2 m/s
  • B. 3 m/s
  • C. 5 m/s
  • D. 7 m/s

Answer: A. 2 m/s

Question 77

Year: 2022 | Marks: 2

The speed of propagation, c, of a capillary wave depends on the density of the fluid, ρ, the wavelength of the wave, λ, and the surface tension, σ. If the density and wavelength remain constant, halving the surface tension would lead to a new velocity, c', given by

  • A. c' = 2c
  • B. c' = √2c
  • C. 𝑐ᇱൌ ௖ √ଶ
  • D. c' = c

Answer: C. 𝑐ᇱൌ ௖ √ଶ

Question 78

Year: 2022 | Marks: 2

A two-dimensional flow field is described by a combination of a source of strength m at the origin and a uniform flow, U, in the positive x-direction such that the velocity potential is given by 2 2 ln 2 y x m Ux + + = π φ The stagnation streamline is shown in the figure. Find the distance a a ′.

Figure for question 78, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. U m
  • B. U m 2
  • C. U m 8
  • D. U m 2

Answer: D. U m 2

Question 79

Year: 2022 | Marks: 2

A typical boundary layer over a flat plate has a linear velocity profile with zero velocity at the wall and freestream velocity, U∞, at the outer edge of the boundary layer. What is the ratio of the momentum thickness to the thickness of the boundary layer?

  • A. 2 1
  • B. 4 1
  • C. 6 1
  • D. 3 1

Answer: C. 6 1

Question 80

Year: 2022 | Type: MSQ | Marks: 2

Identify the configuration(s) in which steady two-dimensional internal flow may show boundary layer separation if the flow direction is left to right.

Figure for question 80, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C. ; D.

Question 81

Year: 2022 | Type: NAT | Marks: 2

Consider steady fully developed flow of a liquid through two large horizontal flat parallel plates separated by a distance of 2 mm. One of the plate is fixed and the other plate moves at a speed of 0.5 m/s. What is the magnitude of the pressure gradient (in Pa/m) in the direction of the flow required to ensure that the net flow through the plates is zero? Dynamic viscosity of the liquid is 5x10-4 Ns/m2 (Round off to the nearest integer)

Answer: 374 to 376

Question 82

Year: 2022 | Type: NAT | Marks: 2

Consider two-dimensional turbulent flow of air over a horizontal flat plate of length 1 m. Skin friction coefficient at a length x from the leading edge of the plate is obtained as: ( ) 2.0 Re 06 .0 x fc = where, Rex is the local Reynolds number. Find out the drag force per unit width (in N/m2) on the plate if the free stream air velocity is 10 m/s. Density and dynamic viscosity of air are given as 1.2 kg/m3 and 1.83x10-5 N-s/m2, respectively. (Round off to three decimal places)

Answer: Marks awarded to all candidates (official key: MTA)

Question 83

Year: 2022 | Type: NAT | Marks: 2

For an inviscid fluid with density 1 kg/m3, the Cartesian velocity field is given as: 𝐮ൌሺെ2𝑥൅𝑦ሻ𝑡𝐢൅ሺ2𝑥൅𝑦ሻ𝑡𝐣 m/s Neglecting the body forces, find the magnitude of pressure gradient in (Pa/m) at (x, y) = (1 m, 1 m) at t = 1 s. (Round off to two decimal places)

Answer: 5.60 to 5.70

Question 84

Year: 2022 | Type: NAT | Marks: 2

Consider a lawn sprinkler with horizontal arms of radius, a = 10 cm which has water introduced vertically through the centre, as shown in the figure. The exit area of the jet is 25 cm2 and the jet velocity is 1 m/s. The water is ejected orthogonal to the sprinkler arm and the jet makes an angle of 60° with the horizontal plane. Find the torque (in N-m) required to hold the sprinkler stationary. Consider water density 1000 kg/m3. Neglect the effects of friction and gravity. (Round off to two decimal places)

Figure for question 84, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.24 to 0.26

Question 85

Year: 2022 | Type: NAT | Marks: 2

A wooden cylinder (specific gravity = 0.6) of length L and diameter D floats in water (density 1000 kg/m3). Find out the minimum value of D/L for which the cylinder floats with its axis vertical. (Round off to three decimal places)

Answer: 1.380 to 1.390

Question 86

Year: 2022 | Type: NAT | Marks: 2

Consider a cart of mass 10 kg placed on an inclined plane (angle of inclination 60° with horizontal) as shown in the figure. A turning vane of negligible weight is mounted on the cart. A horizontal steady water jet is issued from a stationary nozzle of area 0.1 m2 and strikes the turning vane as shown in the figure. The vane turns the jet downward parallel to the inclined plane. Find out the minimum jet velocity (in m/s) which will not allow the cart to come down. Neglect friction, consider density of water = 1000 kg/m3 and acceleration due to gravity = 10 m/s2. (Round off to two decimal places)

Figure for question 86, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.74 to 0.78

Question 87

Year: 2022 | Type: NAT | Marks: 2

A siphon is used to drain out water (density 1000 kg/m3) from a tank as shown in the figure. What can be the maximum height z (in meter) of the point C? Consider acceleration due to gravity = 10 m/s2, pressure at point A = 101 kPa, vapour pressure of water = 29.5 kPa and neglect friction. (Round off to two decimal places)

Figure for question 87, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 5.1 to 5.2

Question 88

Year: 2022 | Type: NAT | Marks: 2

The horizontal belt of negligible weight shown in the figure moves with a steady velocity (V) of 2.5 m/s and skims over the top surface of an oil-film of depth h = 3 cm. The length (L) and width (b) of the belt are, respectively, 2 m and 60 cm. Find the viscosity of the oil (in Pa-s), given that the minimum power required to move the belt is 100 W. Neglect the end effects. (Round off to two decimal places)

Figure for question 88, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.39 to 0.41

Question 89

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.1: see the question image.

Figure for question 89, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 90

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.2: see the question image.

Figure for question 90, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 91

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.3: see the question image.

Figure for question 91, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 92

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.4: see the question image.

Figure for question 92, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 93

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.5: see the question image.

Figure for question 93, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 94

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.6: see the question image.

Figure for question 94, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 95

Year: 2020 | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.7: see the question image.

Figure for question 95, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 96

Year: 2020 | Type: NAT | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.8: see the question image.

Figure for question 96, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.30 to 0.33

Question 97

Year: 2020 | Type: NAT | Marks: 1

GATE XE 2020, Fluid Mechanics, Q.9: see the question image.

Figure for question 97, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 5

Question 98

Year: 2020 | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.10: see the question image.

Figure for question 98, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 99

Year: 2020 | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.11: see the question image.

Figure for question 99, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 100

Year: 2020 | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.12: see the question image.

Figure for question 100, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 101

Year: 2020 | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.13: see the question image.

Figure for question 101, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 102

Year: 2020 | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.14: see the question image.

Figure for question 102, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 103

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.15: see the question image.

Figure for question 103, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 79.60 to 79.90

Question 104

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.16: see the question image.

Figure for question 104, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 183.5 to 184.5

Question 105

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.17: see the question image.

Figure for question 105, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 1.21 to 1.35

Question 106

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.18: see the question image.

Figure for question 106, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 857 to 924

Question 107

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.19: see the question image.

Figure for question 107, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.035 to 0.045

Question 108

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.20: see the question image.

Figure for question 108, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 20

Question 109

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.21: see the question image.

Figure for question 109, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 30.5 to 34.5

Question 110

Year: 2020 | Type: NAT | Marks: 2

GATE XE 2020, Fluid Mechanics, Q.22: see the question image.

Figure for question 110, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Question 111

Year: 2018 | Marks: 1

Rheological diagram of different types of fluids is shown in figure. Column I represents the nature of the fluid and column II represents the curve showing the variation of shear stress against shear strain rate. Column I (i) Newtonian (ii) Shear thinning (iii) Shear thickening (iv) Bingham plastic Column II M N O P The most appropriate match between columns I and II is,

Figure for question 111, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. (i) – O; (ii) – N ; (iii) – P; (iv) – M
  • B. (i) – O; (ii) – P ; (iii) – N; (iv) – M
  • C. (i) – P; (ii) – O ; (iii) – M; (iv) – N
  • D. (i) – P; (ii) – O ; (iii) – N; (iv) – M

Answer: B. (i) – O; (ii) – P ; (iii) – N; (iv) – M

Question 112

Year: 2018 | Marks: 1

In a two-dimensional, incompressible and irrotational flow, stream function ( ( , ) x y ψ ψ = ) and velocity potential ( ( , ) x y φ φ = ) exist. The velocities in x and y directions are non-zero. The product of constant dy dx φ= and constant dy dx ψ= , is

Figure for question 112, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. −1
  • B. 0
  • C. 1
  • D. ∞

Answer: A. −1

Question 113

Year: 2018 | Marks: 1

The inviscid flow past a rotating circular cylinder can be generated by the superposition of

  • A. uniform flow, source and vortex
  • B. uniform flow, doublet
  • C. uniform flow, sink and vortex
  • D. uniform flow, doublet and vortex

Answer: D. uniform flow, doublet and vortex

Question 114

Year: 2018 | Marks: 1

The velocity field and the surface normal vector are given by, ˆ ˆ ˆ V ui v j wk = + + and 1 2 3 ˆ ˆ ˆ n n i n j n k = + + , respectively. If Euler equations are to be solved, the boundary condition that must be satisfied at the wall is,

Figure for question 114, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 𝑉⃗ ∙𝑛⃗ = 0
  • B. 𝑉⃗ = 0
  • C. ∇∙𝑉⃗ = 0
  • D. 𝑉⃗ × 𝑛⃗ = 0

Answer: A. 𝑉⃗ ∙𝑛⃗ = 0

Question 115

Year: 2018 | Marks: 1

The influence of Froude number is most significant in

  • A. capillary flows
  • B. creeping flows
  • C. free surface flows
  • D. compressible flows

Answer: C. free surface flows

Question 116

Year: 2018 | Marks: 1

If the stream function ( ( , ) x y ψ ) for a two-dimensional incompressible flow field is given as ( ) 2 2 2y x y − , the corresponding velocity field is

Figure for question 116, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ( ) 2 2 ˆ ˆ 2 3 4 V x y i xy j = − +
  • B. ( ) 2 2 ˆ ˆ 2 3 4 V x y i xy j = − −
  • C. ( ) 2 ˆ ˆ 2 4 V x y i xy j = −
  • D. ( ) 2 ˆ ˆ 2 4 V x y i xy j = +

Answer: B. ( ) 2 2 ˆ ˆ 2 3 4 V x y i xy j = − −

Question 117

Year: 2018 | Marks: 1

Water is flowing in two different tubes of diameters D and 2D, with the same velocity. The ratio of laminar friction factors for the larger diameter tube to the smaller diameter tube is

  • A. 0.5
  • B. 1.0
  • C. 2.0
  • D. 4.0

Answer: A. 0.5

Question 118

Year: 2018 | Type: NAT | Marks: 1

If the velocity field is 2 ˆ ˆ 4 V xy i xy j = + m/s, vorticity of the fluid element in the field at (x=1, y=2) in s-1 is ____.

Figure for question 118, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 4

Question 119

Year: 2018 | Type: NAT | Marks: 1

A pitot-static tube is used to measure air velocity in a duct by neglecting losses. The density of air is 1.2 kg/m3. If the difference between the total and static pressures is 1 kPa, the velocity of air at the measuring location, in m/s, is _______.

Answer: 39 to 42

Question 120

Year: 2018 | Marks: 2

A parallelepiped of (2 m × 2 m) square cross-section and 10 m in length, is partially floating in water upto a depth of 1.2 m, with its longest side being horizontal. The specific gravity of the block is

  • A. 0.8
  • B. 0.6
  • C. 0.5
  • D. 0.4

Answer: B. 0.6

Question 121

Year: 2018 | Marks: 2

The velocity field in a two-dimensional, unsteady flow is given by 2 ˆ ˆ ( , , ) 2 3 V x y t xy i xyt j = + m/s. The magnitude of acceleration of a fluid particle located at x = 1 m, y = 1 m at the time t = 1 s, in m/s2, is

Figure for question 121, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 16.0
  • B. 18.1
  • C. 24.1
  • D. 34.1

Answer: C. 24.1

Question 122

Year: 2018 | Marks: 2

In a two-dimensional, incompressible and irrotational flow, fluid velocity (v) in the y- direction is given by 2 5 v x y = − . The velocity (u) in the x-direction is

  • A. 2 5 u x y = −
  • B. 2 5 u x y = +
  • C. 5 2 u x y = +
  • D. 5 2 u x y = −

Answer: C. 5 2 u x y = +

Question 123

Year: 2018 | Marks: 2

A two-dimensional laminar viscous liquid film of constant thickness (h) steadily flows down an incline as shown in figure. Acceleration due to gravity is g. If the velocity profile in the liquid film is given as, (2 ); 0 u ky h y v = − = , the value of constant k is

Figure for question 123, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. sin 2 g ρ θ μ
  • B. cos 2 g ρ θ μ
  • C. sin g ρ θ
  • D. cos g ρ θ

Answer: A. sin 2 g ρ θ μ

Question 124

Year: 2018 | Type: NAT | Marks: 2

A water jet of 100 mm diameter issuing out of a nozzle at a speed of 50 m/s strikes a vane and flows along it as shown in figure. The vane is attached to a cart which is moving at a constant speed of 20 m/s on a frictionless track. The jet is deflected at an angle of 30o. Take the density of water as 1000 kg/m3. Neglecting the friction between the vane and the fluid, the magnitude of the force exerted by water on the cart in the x-direction, in N, is ______.

Figure for question 124, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 900 to 990

Question 125

Year: 2018 | Type: NAT | Marks: 2

Capillary waves are generated in the sea. The speed of propagation (C) of these waves is known to be a function of density (ρ), wave length (λ), and surface tension (σ). Assume, ρ and λ to be constant. If the surface tension is doubled, in the functional form of the relevant non-dimensional group, the percentage increase in propagation speed (C) is _______ .

Answer: 40 to 42

Question 126

Year: 2018 | Type: NAT | Marks: 2

Consider a fully developed, two-dimensional and steady flow of a viscous fluid between two fixed parallel plates separated by a distance of 30 mm. The dynamic viscosity of the fluid is 0.01 kg/m-s and the pressure drop per unit length is 300 Pa/m. The fluid velocity at a distance of 10 mm from the bottom plate, in m/s, is ________.

Answer: 2.9 to 3.1

Question 127

Year: 2018 | Type: NAT | Marks: 2

A 2.6 gram smooth table-tennis (ping-pong) ball has a diameter of 38 mm. Density (ρ) of air is 1.2 kg/m3. Neglect the effect of gravity. Take coefficient of drag as 0.5. If the ball is struck with an initial velocity of 30 m/s, the initial deceleration, in m/s2, is _________.

Answer: 107 to 127

Question 128

Year: 2018 | Type: NAT | Marks: 2

On a flat plate, transition from laminar to turbulent boundary layer occurred at a critical Reynolds number (Recr). The empirical relations for the laminar and turbulent boundary layer thickness are given by 0.5 m 5.48Re la x x δ − = and 0.2 0.37Re turb x x δ − = , respectively. The ratio of laminar to turbulent boundary layer thickness, at the location of transition, is 0.3. The value of Recr is _______.

Answer: 440000 to 442000

Question 129

Year: 2018 | Type: NAT | Marks: 2

In a capillary tube of radius R = 0.25 mm, a fully developed laminar velocity profile is defined as, 2 2 2 1 4 R dp r u dx R μ = − − . In this expression, dp dx − =1 MPa/m, μ is the dynamic viscosity of the fluid, and r is the radial position from the centerline of the tube. If the flow rate through the tube is 1000 mm3/s, the viscosity of the fluid, in Pa-s, is ______________.

Answer: 0.001 to 0.002

Question 130

Year: 2018 | Type: NAT | Marks: 2

The skin friction coefficient for a turbulent pipe flow is defined as, 2 1 2 w f C V τ ρ = , where w τ is the wall shear stress and V is the average flow velocity. The value of f C is empirically given by the relation: f C = ( ) 0.25 2 0.065 Re , where Re is the Reynolds number. If the average flow velocity is 10 m/s, diameter of the pipe is 250 mm, kinematic viscosity of the fluid is 0.25×10−6 m2/s, and density of the fluid is 700 kg/m3, the skin friction drag induced by the flow over 1 m length of the pipe, in N, is ___________.

Figure for question 130, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 30 to 45

Question 131

Year: 2018 | Type: NAT | Marks: 2

A (150 mm × 150 mm) square pillar is located in a river with water flowing at a velocity of 2 m/s, as shown in figure. The height of the pillar in water is 8 m. Take density of water as 1000 kg/m3 and kinematic viscosity as 1×10 −6 m/s2. The coefficient of drag of the pillar is 2.0. The drag force exerted by water on the pillar in N is _______.

Figure for question 131, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 4800

Question 132

Year: 2018 | Type: NAT | Marks: 2

An orifice plate is used to measure flow rate of air (density = 1.23 kg/m3) in a duct of 250 mm diameter as shown in figure. The volume flow rate is 1 m3/s. Flow at sections 1 and 3 is uniform and section 2 is located at vena contracta. The diameter ratio, Dt/D1, is 0.66. The flow area at vena contracta, A2 = 0.65At, where At is area of the orifice. The pressure difference between locations 2 and 3 in N/m2 is ____________.

Figure for question 132, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 1200 to 1350

Question 133

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.1: see the question image.

Figure for question 133, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 134

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.2: see the question image.

Figure for question 134, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 135

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.3: see the question image.

Figure for question 135, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 136

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.4: see the question image.

Figure for question 136, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 137

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.5: see the question image.

Figure for question 137, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 138

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.6: see the question image.

Figure for question 138, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 139

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.7: see the question image.

Figure for question 139, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 140

Year: 2017 | Type: NAT | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.8: see the question image.

Figure for question 140, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 22.6

Question 141

Year: 2017 | Marks: 1

GATE XE 2017, Fluid Mechanics, Q.9: see the question image.

Figure for question 141, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 142

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.10: see the question image.

Figure for question 142, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 72.5 to 75.0

Question 143

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.11: see the question image.

Figure for question 143, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 62 to 66

Question 144

Year: 2017 | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.12: see the question image.

Figure for question 144, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 145

Year: 2017 | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.13: see the question image.

Figure for question 145, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 146

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.14: see the question image.

Figure for question 146, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.66 to 0.67

Question 147

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.15: see the question image.

Figure for question 147, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 6005

Question 148

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.16: see the question image.

Figure for question 148, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.05 to 0.06

Question 149

Year: 2017 | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.17: see the question image.

Figure for question 149, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 150

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.18: see the question image.

Figure for question 150, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 1.3 to 1.4

Question 151

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.19: see the question image.

Figure for question 151, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 28.9 to 31.4

Question 152

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.20: see the question image.

Figure for question 152, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.21 to 0.22

Question 153

Year: 2017 | Type: NAT | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.21: see the question image.

Figure for question 153, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 7.0 to 7.2

Question 154

Year: 2017 | Marks: 2

GATE XE 2017, Fluid Mechanics, Q.22: see the question image.

Figure for question 154, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 155

Year: 2016 | Type: NAT | Marks: 1

In the parallel-plate configuration shown, steady-flow of an incompressible Newtonian fluid is established by moving the top plate with a constant speed, U0 = 1m/s. If the force required on the top plate to support this motion is 0.5 N per unit area (in m2) of the plate then the viscosity of the fluid between the plates is __________ N-s/m2

Figure for question 155, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.0049 to 0.0051

Question 156

Year: 2016 | Marks: 1

For a newly designed vehicle by some students, volume of fuel consumed per unit distance travelled (qf in m3/m) depends upon the viscosity (μ) and density (ρ) of the fuel and, speed (U) and size (L) of the vehicle as where C is a constant. The dimensions of the constant C are

Figure for question 156, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. M0L0T0
  • B. M2L-1T-1
  • C. M2L-5T-1
  • D. M-2L1T1

Answer: B. M2L-1T-1

Question 157

Year: 2016 | Type: NAT | Marks: 1

A semi-circular gate of radius 1m is placed at the bottom of a water reservoir as shown in figure below. The hydrostatic force per unit width of the cylindrical gate in y-direction is _______ kN. The gravitational acceleration, g = 9.8 m/s2 and density of water = 1000 kg/m3.

Figure for question 157, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 15.3 to 15.5

Question 158

Year: 2016 | Type: NAT | Marks: 1

Velocity vector in m/s for a 2-D flow is given in Cartesian coordinate as Symbols bear usual meaning. At a point in the flow field, the - and -components of the acceleration vector are given as m/s2 and -0.5 m/s2, respectively. The velocity magnitude at that point is ________ m/s.

Figure for question 158, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 1.4 to 1.42

Question 159

Year: 2016 | Marks: 1

If is velocity potential and is stream function for a 2-D, steady, incompressible and irrotational flow, which one of the followings is incorrect?

Figure for question 159, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B. + = 0
  • C.
  • D. + = 0

Answer: C.

Question 160

Year: 2016 | Marks: 1

The flow field shown over a bluff body has considerably curved streamlines. A student measures pressures at points A, B, C, and D and denotes them as PA, PB, PC, and PD respectively. State which one of the following statements is true. The arrow indicates the freestream flow direction.

Figure for question 160, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. PA = PB and PC > PD
  • B. PA > PB and PC > PD
  • C. PA = PB and PC < PD
  • D. PA > PB and PC < PD

Answer: D. PA > PB and PC < PD

Question 161

Year: 2016 | Type: NAT | Marks: 1

A 2-D incompressible flow is defined by its velocity components in m/s as and . If the value of the constant is equal to 0.1 m2/s, the numerical value of vorticity at the point m and m is ________ s-1.

Figure for question 161, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: -0.00001 to 0.00001

Question 162

Year: 2016 | Marks: 1

Two flow configurations are shown below for flow of incompressible, viscous flow. The inlet velocity for the diverging nozzle (Fig (i)) and free-stream velocity for flow past the bluff body (Fig(ii)) is constant. Points A and B are separation points and flow is laminar. The relation regarding velocity gradients at point A and B is (y is the direction normal to the surface at the point of separation)

Figure for question 162, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D. )

Answer: A.

Question 163

Year: 2016 | Type: NAT | Marks: 1

Consider a fully developed, steady, incompressible, 2-D, viscous channel flow with uniform suction and blowing velocity , as shown in the figure given below. The centerline velocity of the channel is 10 m/s along the x-direction. If the value of at both the walls is 1 m/s, the value of the y- component of velocity inside the flow field is __________ m/s.

Figure for question 163, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.9 to 1.1

Question 164

Year: 2016 | Type: NAT | Marks: 2

Exhaust from a kitchen goes into the atmosphere through a tapered chimney as shown. The area of cross-section of chimney at location-1 is twice of that at location-2. The flow can be assumed to be inviscid with constant exhaust density of 1 kg/m3 and acceleration due to gravity, g = 9.8 m/s2. If the steady, uniform exhaust velocity at location-1 is U = 1m/s, the pressure drop across the chimney is ________ Pa.

Figure for question 164, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 2.95 to 3.05

Question 165

Year: 2016 | Type: NAT | Marks: 2

A jet of diameter 20 mm and velocity 6 m/s coming out of a water-tank standing on a frictionless cart hits a vane and gets deflected at an angle 45o as shown in the figure below. The density of water is 1000 kg/m3. Neglect all minor and viscous losses. If the cart remains stationary, the magnitude of tension in the supporting string connected to the wall is ________ N.

Figure for question 165, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 7.9 to 8.1

Question 166

Year: 2016 | Type: NAT | Marks: 2

A block is floating at the oil-water interface as shown. The density of oil is two-thirds of that of water. Given that the density of the block is 800 kg/m3 and that of water is 1000 kg/m3, the fraction of the total height of block in oil is ________.

Figure for question 166, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.59 to 0.61

Question 167

Year: 2016 | Type: NAT | Marks: 2

A horizontal pipe is feeding water into a reservoir from the top with a time-dependent volumetric flow-rate, Q (m3/h)= 1+0.1 where t is time in hours. The area of the base of the reservoir is 0.5 m2. Assuming that initially the reservoir was empty, the height of the water level in the reservoir after 60 minutes is __________ m.

Figure for question 167, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 2.09 to 2.11

Question 168

Year: 2016 | Marks: 2

Velocity field of a 2-D steady flow is provided as = . The equation of the streamlines of this flow is

Figure for question 168, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 169

Year: 2016 | Marks: 2

Velocity potential and stream function in polar coordinates ( r, θ ) for a potential flow over a cylinder with radius is given as and , respectively. Here, denotes uniform freestream velocity, and θ is measured counter clockwise as shown in the figure. How does the velocity magnitude, , over the surface of the cylinder will vary?

Figure for question 169, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: D.

Question 170

Year: 2016 | Type: NAT | Marks: 2

Consider a laminar flow over a flat plate of length = 1m. The boundary layer thickness at the end of the plate is for water, and for air for the same freestream velocity. If the kinematic viscosities of water and air are 1 and 1 , respectively, the numerical value of the ratio, is _________.

Figure for question 170, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.24 to 0.26

Question 171

Year: 2016 | Marks: 2

Prototype of a dam spillway ( a structure used for controlled release of water from the dam) has characteristic length of 20m and characteristic velocity of 2 m/s. A small model is constructed by keeping Froude number same for dynamic similarity between the prototype and the model. What is the minimum length-scale ratio between prototype and the model such that the minimum Reynolds' number for the model is 100? The density of water is 1000 kg/m3 and viscosity is 10-3 Pa-s.

Figure for question 171, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1.8 10-4
  • B. 1 10-4
  • C. 1.8 10-3
  • D. 9.1 10-4

Answer: A. 1.8 10-4

Question 172

Year: 2016 | Type: NAT | Marks: 2

An orifice meter, having orifice diameter of d is placed in a water pipeline having flow rate, . The ratio of orifice diameter to pipe diameter is 0.6. The contraction coefficient is also 0.6. The density of water is 1000 kg/m3. If the pressure drop across the orifice plate is 43.5kPa, the discharge co-efficient of the orifice meter at this flow Reynolds number is _________.

Figure for question 172, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.29 to 0.33

Question 173

Year: 2016 | Marks: 2

Consider the following figures shown below. The objects are marked as A1, A2, B1, B2 and C1, C2 and the flow directions over these objects are shown by the respective arrow placed to the left of the object. Freestream velocities are same for all the cases. Amongst these objects, A1, A2, B1 and C1 are having smooth surfaces while B2 and C2 are having rough surfaces. Reynolds number is such that flow over rough surfaces become turbulent and flow over smooth surfaces can be considered laminar. All the airfoils can be considered as thin slender airfoil. Among the statements (i) to (vi) made about the drag of these objects which is/are correct? (i) Drag of object A1 is less than drag of object A2. (ii) Drag of Object A1 and A2 are same. (iii) Drag of Object B1 is more than drag of object B2. (iv) Drag of object B2 is more than drag of object B1. (v) Drag of Object C1 is more than drag of object C2. (vi) Drag of object C2 is more than drag of object C1.

Figure for question 173, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. (i),(iii) & (vi)
  • B. (ii),(iii) & (vi)
  • C. (i),(iii) & (v)
  • D. (i),(iv) & (vi)

Answer: A. (i),(iii) & (vi)

Question 174

Year: 2016 | Type: NAT | Marks: 2

Consider 2-D, steady, incompressible, fully developed flow of viscous, Newtonian fluid through two stationary parallel plates, in Cartesian co-ordinate (x,y,z) system. Assume plates are very long in x-direction, wide in z-direction (also there is no variation of velocity in z direction) and distance between them is 2h. The velocity in such a channel is given as The origin y = 0 is located at the center between the plates. If h = 48 mm and , difference between values of stream functions passing through y = 0 and y = h/2 is __________ mm2/s.

Figure for question 174, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 2190 to 2210

Question 175

Year: 2016 | Type: NAT | Marks: 2

A pump is used to deliver water to an overhead tank at a flow rate of . The pump adds1.6 kW to water. If the density of water is 1000 kg/m3 and acceleration due to gravity is 10 m/s2, the pump head added to the flow is _________ m.

Figure for question 175, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 39 to 41

Question 176

Year: 2016 | Type: NAT | Marks: 2

Water is discharged at atmospheric pressure from a large reservoir through a long pipe of diameter d and length L. The height of the free surface of the reservoir from the discharge point is h meters. The Darcy's friction factor of the pipe is 0.002. Neglect the velocity inside the reservoir as the reservoir is very large. Given, L = 20m, d = 40mm, density of water = 1000kg/m3 and flow rate is . Assume gravitational acceleration, g = 10 m/s2. The value of h is _______m.

Figure for question 176, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 9.7 to 10.3

Question 177

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.1: see the question image.

Figure for question 177, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 178

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.2: see the question image.

Figure for question 178, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
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  • D.

Answer: A.

Question 179

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.3: see the question image.

Figure for question 179, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 180

Year: 2015 | Type: NAT | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.4: see the question image.

Figure for question 180, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: -2.4 to -2.2

Question 181

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.5: see the question image.

Figure for question 181, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

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  • B.
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  • D.

Answer: D.

Question 182

Year: 2015 | Type: NAT | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.6: see the question image.

Figure for question 182, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 5.5 to 5.7

Question 183

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.7: see the question image.

Figure for question 183, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

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  • B.
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  • D.

Answer: A.

Question 184

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.8: see the question image.

Figure for question 184, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

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  • B.
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  • D.

Answer: C.

Question 185

Year: 2015 | Marks: 1

GATE XE 2015, Fluid Mechanics, Q.9: see the question image.

Figure for question 185, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
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  • D.

Answer: B.

Question 186

Year: 2015 | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.10: see the question image.

Figure for question 186, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 187

Year: 2015 | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.11: see the question image.

Figure for question 187, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: A.

Question 188

Year: 2015 | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.12: see the question image.

Figure for question 188, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: B.

Question 189

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.13: see the question image.

Figure for question 189, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 7.9 to 8.1

Question 190

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.14: see the question image.

Figure for question 190, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 0.7 to 0.8

Question 191

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.15: see the question image.

Figure for question 191, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 14 to 16

Question 192

Year: 2015 | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.16: see the question image.

Figure for question 192, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

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  • B.
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  • D.

Answer: D.

Question 193

Year: 2015 | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.17: see the question image.

Figure for question 193, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Answer: C.

Question 194

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.18: see the question image.

Figure for question 194, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 23 to 25

Question 195

Year: 2015 | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.19: see the question image.

Figure for question 195, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
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  • D.

Answer: D.

Question 196

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.20: see the question image.

Figure for question 196, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 2.5 to 2.7

Question 197

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.21: see the question image.

Figure for question 197, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 1.5 to 1.7

Question 198

Year: 2015 | Type: NAT | Marks: 2

GATE XE 2015, Fluid Mechanics, Q.22: see the question image.

Figure for question 198, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 205 to 210

Question 199

Year: 2014 | Type: NAT | Marks: 1

A dam with a curved shape is shown in the figure. The cross sectional area of the dam (shaded portion) is 100 m2 and its centroid is at 10 x = m. The vertical component of the hydrostatic force, zF , is acting at a distance p x . The value of p x is ____ m.

Figure for question 199, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 7

Question 200

Year: 2014 | Marks: 1

For an unsteady incompressible fluid flow, the velocity field is ( ) 2 ˆ ˆ 3 3 6 V x t i xyt j = + − ρ , where x , y are in meters and t is in seconds. Acceleration in m/s2 at the point 10 x = m and 0 y = , as measured by a stationary observer is

  • A. 303
  • B. 162
  • C. 43
  • D. 13

Answer: A. 303

Question 201

Year: 2014 | Marks: 1

For an incompressible flow, the existence of components of acceleration for different types of flow is described in the table below. Type of Flow Components of Acceleration P: Steady and uniform 1: Local exists, convective does not exist Q: Steady and non-uniform 2: Both exist R: Unsteady and uniform 3: Both do not exist S: Unsteady and non-uniform 4: Local does not exist, convective exists Which one of the following options connecting the left column with the right column is correct?

  • A. P – 1; Q – 4; R – 3; S – 2
  • B. P – 4; Q – 1; R – 2; S – 3
  • C. P – 3; Q – 2; R – 1; S – 4
  • D. P – 3; Q – 4; R – 1; S – 2 15 m 40 m O G px x x z zF XE (GATE 2014)

Answer: D. P – 3; Q – 4; R – 1; S – 2 15 m 40 m O G px x x z zF XE (GATE 2014)

Question 202

Year: 2014 | Type: NAT | Marks: 1

Velocity in a two-dimensional flow field is specified as: 2 2 ; u x y v y x = = − . The magnitude of the rate of angular deformation at a location ( 2 x = m and 1 y = m) is ____ s-1.

Answer: 3

Question 203

Year: 2014 | Marks: 1

For a plane irrotational flow, equi-potential lines and streamlines are

  • A. parallel to each other.
  • B. at an angle of 90o to each other.
  • C. at an angle of 45o to each other.
  • D. at an angle of 60o to each other.

Answer: B. at an angle of 90o to each other.

Question 204

Year: 2014 | Marks: 1

Flow around a Rankine half-body is represented by the superposition of

  • A. source and vortex flows.
  • B. source and uniform flows.
  • C. vortex and uniform flows.
  • D. source, vortex and uniform flows.

Answer: B. source and uniform flows.

Question 205

Year: 2014 | Type: NAT | Marks: 1

It is required to carry out model studies on a boat having a characteristic length of 3.6 m and travelling at a speed of 3 m/s. Assume the acceleration due to gravity as 10 m/s2 and neglect the effects due to viscous and surface tension forces. The value of appropriate non-dimensional number is ____.

Answer: 0.48 to 0.52

Question 206

Year: 2014 | Marks: 1

Which one of the following velocity profiles typically represents a fully developed incompressible, turbulent flow in a pipe?

Figure for question 206, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D. XE (GATE 2014)

Answer: C.

Question 207

Year: 2014 | Marks: 1

Consider an incompressible, laminar flow past a circular cylinder of diameter d . The flow is uniform at the far upstream. Which one of the following figures typically represents the wake velocity profile just downstream of the cylinder?

Figure for question 207, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D. d d d d XE (GATE 2014)

Answer: C.

Question 208

Year: 2014 | Marks: 2

A container of square cross-section is partially filled with a liquid of density 1 ρ . The cylinder is intended to float in another liquid of density 2 ρ as shown in the figure. The distance between metacentre and centre of buoyancy is sub I V , where I and sub V are area moment of inertia of the cross-section and submerged volume, respectively. Neglect the weight of the container. Which one of the following is the correct condition for stability?

Figure for question 208, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 2 1 1 2 1 0 6 b h h b ρ ρ ρ ρ − − >
  • B. 2 1 1 2 1 0 6 b h h b ρ ρ ρ ρ − + >
  • C. 2 1 1 2 1 0 6 b h h b ρ ρ ρ ρ + − >
  • D. 2 1 1 2 1 0 6 b h h b ρ ρ ρ ρ + + >

Answer: A. 2 1 1 2 1 0 6 b h h b ρ ρ ρ ρ − − >

Question 209

Year: 2014 | Marks: 2

In a steady state two-dimensional potential flow field due to a point source, the acceleration of a particle at a distance r from the point source is

  • A. proportional to 1 r−.
  • B. proportional to r .
  • C. a constant.
  • D. proportional to 3 r −.

Answer: D. proportional to 3 r −.

Question 210

Year: 2014 | Marks: 2

Velocity in a two-dimensional flow at time t and location ( ) ,x y is described as: ( ) 2 ˆ ˆ 3 1 V t i x j = + − ρ . The equation for the path line of a particle passing through the point (1,0) at 0 t = is

  • A. 4 3 4 0 x y − =
  • B. ( ) 3 4 1 2 0 x y − − =
  • C. ( ) 4 3 1 64 0 x y − − =
  • D. ( ) 4 3 1 16 0 x y + − = h b XE (GATE 2014)

Answer: C. ( ) 4 3 1 64 0 x y − − =

Question 211

Year: 2014 | Marks: 2

The gravity driven flow over a hump of height h in a canal is shown in the figure. The height of the free surface from the canal bed at upstream of the hump is H . The free surface height reduces to 1 H above the hump. Assuming the canal bed to be horizontal, the discharge per unit width is given by

Figure for question 211, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ඩ 2𝑔𝑔(𝐻𝐻−𝐻𝐻1 −ℎ) 1 𝐻𝐻1 2 −1 𝐻𝐻2
  • B. ඩ 2𝑔𝑔ℎ 1 (𝐻𝐻1 + ℎ)2 −1 𝐻𝐻2
  • C. ඩ 2𝑔𝑔(𝐻𝐻−𝐻𝐻1) 1 (𝐻𝐻1 + ℎ)2 −1 𝐻𝐻2
  • D. ඩ 2𝑔𝑔(𝐻𝐻−𝐻𝐻1) 1 𝐻𝐻1 2 −1 𝐻𝐻2

Answer: A. ඩ 2𝑔𝑔(𝐻𝐻−𝐻𝐻1 −ℎ) 1 𝐻𝐻1 2 −1 𝐻𝐻2

Question 212

Year: 2014 | Type: NAT | Marks: 2

Steady state incompressible flow through a pipe network is shown in the figure. Inlets marked as (1), (2) and (3) and exit marked as (4), are shown with their respective diameters. The exit flow rate at (4) is 0.1 m3/s. A 20% increase in flow rate through (3) results in a 10% increase in flow rate through (4). The original velocity through inlet (3) is _____ m/s. H h 1 H 5 cm 10 cm (3) (2) (1) (4) XE (GATE 2014)

Figure for question 212, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 17.55 to 17.75

Question 213

Year: 2014 | Type: NAT | Marks: 2

A reducing elbow is used to deflect water upward by 30o as shown in the figure. The mass flow rate at the inlet is 14 kg/s. Water is entering at a gauge pressure of 200 kPa and exits to the atmosphere. The cross-sectional area is 113 cm2 at the inlet and 7 cm2 at the exit. Density of water and acceleration due to gravity are 1000 kg/m3 and 10 m/s2, respectively. Magnitude of x - component of the water force on the elbow is ____ N.

Figure for question 213, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 2033 to 2036

Question 214

Year: 2014 | Marks: 2

A source with a strength of 1k and a vortex with a strength of 2k are located at the origin. The resultant velocity at a radial distance r from the origin due to the superposition of the source and vortex is expressed as

Figure for question 214, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1 2 k k r +
  • B. 2 2 1 2 k k r +
  • C. 2 2 1 2 k k r −
  • D. 1 2 k k r −

Answer: B. 2 2 1 2 k k r +

Question 215

Year: 2014 | Type: NAT | Marks: 2

Velocity potential for an incompressible fluid flow is given as: ( ) 2 2 2 2 x y y φ = + − . Assume the value of stream function at the origin to be zero. The value of stream function at [( ) ( ) , 2,2 x y ≡ ] is ____.

Answer: 8

Question 216

Year: 2014 | Type: NAT | Marks: 2

The model of a conduit is scaled to 1/100 of the actual size. Seawater is used in the prototype and fresh water is used in the model. Velocity in the prototype is 0.5 m/s. Density and dynamic viscosity of the seawater are 1025 kg/m3 and 1.07 × 10-3 kg/m-s, respectively. Density and dynamic viscosity of fresh water are 1000 kg/m3 and 1 × 10-3 kg/m-s, respectively. Assume the viscous forces to be dominant. The velocity to be maintained in the model to ensure dynamic similarity is____ m/s.

Answer: 47.52 to 48.50

Question 217

Year: 2014 | Type: NAT | Marks: 2

A fluid is flowing through a pipe of circular cross-section. Reynolds number of the flow is 1600. The head loss over a 45 m length of the pipe is 0.6 m. The average flow velocity of the fluid is 1 m/s and the acceleration due to gravity is 10 m/s2. The diameter of the pipe is ____ m. XE (GATE 2014)

Answer: 0.145 to 0.155

Question 218

Year: 2014 | Marks: 2

Consider a laminar flow over a flat plate of width w . At Section 1-1, the velocity profile is uniform as shown in the figure. The x -direction velocity profile at Section 2-2 is given by 2 2 , u y y U δ δ = − where δ is the boundary layer thickness. The volume flow rate through Section 2-2 is given by

Figure for question 218, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1 2U wδ
  • B. 1 3U wδ
  • C. U wδ
  • D. 2 3U wδ

Answer: D. 2 3U wδ

Question 219

Year: 2014 | Marks: 2

A cube of weight W and side a falls at a constant speed in a medium as shown in the figure. If the medium is air (mass density =𝜌𝜌air ) let air U be the velocity of the cube. If the medium is water (mass density =𝜌𝜌water ) let water U be the velocity of the cube. Neglecting the buoyancy force and assuming drag coefficient to be same for both cases, the ratio of velocities, air water U U is given by

Figure for question 219, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. air water ρ ρ
  • B. air water ρ ρ
  • C. water air ρ ρ
  • D. 1 δ 1 1 2 2 U U ( ) u y x y a W XE (GATE 2014)

Answer: C. water air ρ ρ

Question 220

Year: 2014 | Type: NAT | Marks: 2

Water is flowing through a venturimeter having a diameter of 0.25 m at the entrance (Station 1) and 0.125 m at the throat (Station 2) as shown in the figure. A mercury manometer measures the piezometric head difference between Stations 1 and 2 as 1.3505 m. The loss of head between these two stations, is 1/7 times the velocity head at the Station 2. Assume the acceleration due to gravity to be 10 m/s2. The velocity of water at the throat is ____ m/s. • • 1 2 diameter 0.125 m diameter 0.25m Mercury Manometer XE (GATE 2014)

Figure for question 220, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Answer: 4.8 to 5.2

Question 221

Year: 2013 | Marks: 1

The gauge pressure inside a soap bubble of radius ܴ, with ߪ denoting the surface tension between the soap solution and air, is.

Figure for question 221, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ఙ ଶగோ
  • B. ସఙ ோ
  • C. ଶఙ ோ
  • D. ఙ ସగோ

Question 222

Year: 2013 | Marks: 1

Let ܯ, ܤ and ܩ represent respectively the metacentre, centre of buoyancy and the centre of mass of a floating buoy. Which of the following statements is correct?

  • A. ܯ is above ܩ; Buoy unstable
  • B. ܤ is above ܩ; Buoy stable
  • C. ܯ is above ܩ; Buoy stable
  • D. ܤ is above ܩ; Buoy unstable

Question 223

Year: 2013 | Type: NAT | Marks: 1

A reservoir connected to a pipe line is being filled with water, as shown in the Figure. At any time t, the free surface level in the reservoir is h. Find the time in seconds for the reservoir to get filled up to a height of 1 m, if the initial level is 0.2 m. _________

Figure for question 223, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Question 224

Year: 2013 | Marks: 1

Bernoulli’s equation is valid for the following type of flow:

  • A. Compressible, steady, inviscid
  • B. Incompressible, steady, viscous
  • C. Compressible, unsteady, viscous
  • D. Incompressible, steady, inviscid

Question 225

Year: 2013 | Marks: 1

If ܣ is the area of a circle of radius ݎ enclosing a plane forced vortex flow, with origin at the centre of the vortex and if ω is the angular velocity, ζ is the vorticity, ܸሬ⃗ is the velocity vector, then the circulation around the contour of the circle is given by

  • A. 2߱ܣ
  • B. 2ζܣ
  • C. 2ܸሬ⃗ܣ
  • D. 0

Question 226

Year: 2013 | Marks: 1

Flow past a circular cylinder can be produced by superposition of the following elementary potential flows:

  • A. Uniform flow, doublet
  • B. Uniform flow, vortex
  • C. Source, vortex
  • D. Sink, vortex

Question 227

Year: 2013 | Marks: 1

Let δ, δ1 and δ2 denote respectively the boundary-layer thickness, displacement thickness and the momentum thickness for laminar boundary layer flow of an incompressible fluid over a flat plate. The correct relation among these quantities is

  • A. δ < δ1< δ2
  • B. δ > δ1> δ2
  • C. δ > δ1< δ2
  • D. δ < δ1> δ2

Question 228

Year: 2013 | Marks: 1

In the hydrodynamic entry region of a circular duct, the pressure forces balance the sum of

  • A. viscous and buoyancy forces
  • B. inertia and buoyancy forces
  • C. inertia and surface tension forces
  • D. inertia and viscous forces

Question 229

Year: 2013 | Marks: 1

Bodies with various cross-sectional shapes subjected to cross-flow of air are shown in the following figures. The characteristic dimension of all the shapes is the same. The cross- sectional shape with the largest coefficient of drag (i.e. sum of the pressure and skin- friction drags), at any moderately large Reynolds number, is

Figure for question 229, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A.
  • B.
  • C.
  • D.

Question 230

Year: 2013 | Marks: 2

A U-tube of a very small bore, with its limbs in a vertical plane and filled with a liquid of density ρ, up to a height of h, is rotated about a vertical axis, with an angular velocity of ω, as shown in the Figure. The radius of each limb from the axis of rotation is R. Let pa be the atmospheric pressure and g, the gravitational acceleration. The angular velocity at which the pressure at the point O becomes half of the atmospheric pressure is given by

Figure for question 230, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ට ௣ೌାଶఘ௚௛ ఘோమ
  • B. ට ଶ(௣ೌାఘ௚௛) ఘோమ
  • C. ට ௣ೌାଶఘ௚௛ ଶఘோమ
  • D. ට ௣ೌାఘ௚௛ ଶఘோమ

Question 231

Year: 2013 | Marks: 2

An incompressible fluid at a pressure of 150 kPa (absolute) flows steadily through a two- dimensional channel with a velocity of 5 m/s as shown in the Figure. The channel has a 90o bend. The fluid leaves the channel with a pressure of 100 kPa (absolute) and linearly- varying velocity profile. vmax is four times vmin. The density of the fluid is 914.3 kg/m3. The velocity vmin, in m/s, is

Figure for question 231, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 25
  • B. 2.5
  • C. 2.0
  • D. 0.2

Question 232

Year: 2013 | Marks: 2

The velocity vector corresponding to a flow field is given, with usual notation, by ܸሬ⃗= 3ݔଓ̂ + 4ݔݕଔ̂. The magnitude of rotation at the point (2,2) in rad/s is

Figure for question 232, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 0.75
  • B. 1.33
  • C. 2
  • D. 4

Question 233

Year: 2013 | Marks: 2

The stream function for a potential flow field is given by ψ = ݔଶ−ݕଶ. The corresponding potential function, assuming zero potential at the origin, is

Figure for question 233, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ݔଶ+ ݕଶ
  • B. 2ݔݕ
  • C. ݔଶ−ݕଶ
  • D. ݔ−ݕ

Question 234

Year: 2013 | Type: NAT | Marks: 2

Fully developed flow of an oil takes place in a pipe of inner diameter 50 mm. The pressure drop per metre length of the pipe is 2 kPa. Determine the shear stress, in Pa, at the pipe wall. __________

Question 235

Year: 2013 | Type: NAT | Marks: 2

The Darcy friction factor ݂ for a smooth pipe is given by = 64/Re for laminar flow and by = 0.3/Re଴.ଶହfor turbulent flow, where Re is the Reynolds number based on the diameter. For fully developed flow of a fluid of density 1000 kg/m3 and dynamic viscosity 0.001 Pa.s through a smooth pipe of diameter 10 mm with a velocity of 1 m/s, determine the Darcy friction factor. _________

Figure for question 235, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Question 236

Year: 2013 | Type: NAT | Marks: 2

Air flows steadily through a channel. The stagnation and static pressures at a point in the flow are measured by a Pitot tube and a wall pressure tap, respectively. The pressure difference is found to be 20 mm Hg. The densities of air, water and mercury, in kg/m3, are 1.18, 1000 and 13600, respectively. The gravitational acceleration is 9.81 m/s2. Determine the air speed in m/s. _____________

Question 237

Year: 2013 | Type: NAT | Marks: 2

Calculate the x-direction component of the acceleration in m/s2 at the point ݔ= 0.5 m and ݕ= 50 mm. _________

Figure for question 237, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Question 238

Year: 2013 | Type: NAT | Marks: 2

Find the slope of the streamline passing through the point ݔ= 0.5 m and ݕ= 50mm. ____

Figure for question 238, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

Question 239

Year: 2013 | Marks: 2

The velocity in m/s, at which the model is towed, is

Figure for question 239, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 0.75
  • B. 1.33
  • C. 3
  • D. 192

Question 240

Year: 2013 | Marks: 2

The resistance of the prototype, in kN, is

Figure for question 240, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 6
  • B. 25
  • C. 26.9
  • D. 100.1

Question 241

Year: 2013 | Marks: 2

The gauge pressure at section-1, in kPa, is

Figure for question 241, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 0.6
  • B. 13.5
  • C. 135
  • D. 600

Question 242

Year: 2013 | Marks: 2

The magnitude of the force, in kN, required to hold the pipe in place, is

Figure for question 242, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 2.7
  • B. 5.4
  • C. 19
  • D. 27

Question 243

Year: 2012 | Marks: 1

In a two-dimensional flow field, the velocities in the x- and y- directions are u and v, respectively. The shear stress for a Newtonian fluid having dynamic viscosity µ is given by

Figure for question 243, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. ∂ ∂ − ∂ ∂ y u x v μ
  • B. y v ∂ ∂ μ 2
  • C. x u ∂ ∂ μ 2
  • D. ∂ ∂ + ∂ ∂ y u x v μ

Answer: D. ∂ ∂ + ∂ ∂ y u x v μ

Question 244

Year: 2012 | Marks: 1

In a potential flow, the superposition of the stream functions of a uniform flow and a line source gives rise to a dividing streamline representing

  • A. Rankine’s half-body
  • B. infinite circular cylinder
  • C. infinite rotating circular cylinder
  • D. infinite elliptical cylinder

Answer: A. Rankine’s half-body

Question 245

Year: 2012 | Marks: 1

Given that V, L and g are the characteristic velocity, characteristic length and acceleration due to gravity, respectively, the expression Lg V represents

Figure for question 245, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. Weber number
  • B. Euler number
  • C. Cavitation number (D) Froude number
  • D.

Answer: D.

Question 246

Year: 2012 | Marks: 1

Match the devices in Column I with the characteristics in Column II. Column I Column II P. orifice meter 1. high head loss and low cost Q. venturi meter 2. high head loss and high cost 3. low head loss and high cost 4. low head loss and low cost

  • A. P − 2; Q − 4
  • B. P − 1; Q − 2
  • C. P − 3; Q − 1
  • D. P − 1; Q − 3

Answer: D. P − 1; Q − 3

Question 247

Year: 2012 | Marks: 1

Identify the visualization method that shows a PATHLINE in an unsteady flow, assuming that the camera covers the required field of view.

  • A. A dye is continuously injected and a snap shot is taken
  • B. A dye is continuously injected and a long-exposure picture is taken
  • C. A blob (or drop) of dye is injected and a snap shot is taken
  • D. A blob (or drop) of dye is injected and a long-exposure picture is taken

Answer: D. A blob (or drop) of dye is injected and a long-exposure picture is taken

Question 248

Year: 2012 | Marks: 1

In the case of a fully developed flow through a pipe, the shear stress at the centerline is

  • A. a function of the axial distance
  • B. a function of the centerline velocity
  • C. zero
  • D. infinite

Answer: C. zero

Question 249

Year: 2012 | Marks: 1

The velocity in a one-dimensional unsteady flow is given by (x2 − t), where x is the position and t is the time. The total acceleration at any x and t is

  • A. −1 + x t + x3
  • B. −1 + x t + 2 x3
  • C. −1 − x t − x3
  • D. −1 − 2 x t + 2 x3

Answer: D. −1 − 2 x t + 2 x3

Question 250

Year: 2012 | Marks: 1

If ψ is the stream function, the Laplace’s equation 0 2 = ∇ψ is true when the flow is

Figure for question 250, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. incompressible
  • B. incompressible and irrotational
  • C. irrotational
  • D. compressible

Answer: B. incompressible and irrotational

Question 251

Year: 2012 | Marks: 1

A fully developed laminar flow is taking place through a pipe. If the flow velocity is doubled maintaining the flow laminar, the pressure loss would be

  • A. halved
  • B. unaltered
  • C. doubled
  • D. trebled

Answer: C. doubled

Question 252

Year: 2012 | Marks: 2

In the following equations, u and v are the velocities in the x- and y- directions, respectively and t is time. The flow field that CANNOT be termed as incompressible is

Figure for question 252, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. , 3 2 3 2 u = x + x y v = y + y x
  • B. 10 , 10 u = xt v = yt −
  • C. ( ) ( ) 1/7 / , 0 constant u = y v = δ δ=
  • D. 2 , 2 u = y v = x

Answer: A. , 3 2 3 2 u = x + x y v = y + y x

Question 253

Year: 2012 | Marks: 2

A U-tube mercury (Hg) manometer as shown below is employed to measure the pressure of an oil-filled vessel. The densities of Hg and oil are 13600 kg/m3 and 800 kg/m3, respectively. The gravitational acceleration may be taken as 10 m/s2. The gauge pressure (in Pa) at point A when h1 = 0.5 m and h2 = 0.9 m, is approximately

Figure for question 253, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 3 118.4 10 ×
  • B. 118.4
  • C. 11.84
  • D. 1.184

Answer: A. 3 118.4 10 ×

Question 254

Year: 2012 | Marks: 2

Water is supplied to a tank at the rate of 0.02 m3/s, as shown in the figure below. The cross- sectional area of the tank is 1 m2 and the inner diameter of the outlet pipe is 60 mm. At a time when the water level in the tank is increasing at the rate of 5 mm/s, the average velocity (in m/s) of water in the outlet pipe is approximately

Figure for question 254, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 0.005
  • B. 0.06
  • C. 5.3
  • D. 20 Water supply Tank water level Outlet pipe h2 h1 Atmosphere Hg

Answer: C. 5.3

Question 255

Year: 2012 | Marks: 2

The water level in a gas-pressurized tank with a large cross-sectional area is maintained constant as shown in the figure below. The water level in the tank is 4.2 m above the pipe centerline as indicated in the figure. The gas pressure is 130 kPa. The atmospheric pressure, gravitational acceleration and density of water may be taken as 100 kPa, 10 m/s2 and 1000 kg/m3, respectively. Neglecting losses, the maximum velocity (in m/s) of water at any location in the horizontal portion of the delivery pipe for the pressure NOT to drop below atmospheric pressure, is

Figure for question 255, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1.3
  • B. 4.2
  • C. 10
  • D. 12

Answer: D. 12

Question 256

Year: 2012 | Marks: 2

The figure given below shows typical non-dimensional velocity profiles for fully developed laminar flow between two infinitely long parallel plates separated by a distance a along y-direction. The upper plate is moving with a constant velocity U in the x-direction and the lower plate is stationary. Match the non-dimensional velocity profiles in Column I with the pressure gradients in Column II. Column I Column II P. profile I 1. 0 p x ∂ > ∂ Q. profile II 2. 0 p x ∂ < ∂ R. profile III 3. 0 p x ∂ = ∂

Figure for question 256, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. P − 2; Q − 3; R − 1
  • B. P − 3; Q − 2; R − 1
  • C. P − 3; Q − 1; R − 2
  • D. P − 1; Q − 2; R − 3 -3 -2 -1 0 1 2 3 0 1 u/U I II III a y

Answer: A. P − 2; Q − 3; R − 1

Question 257

Year: 2012 | Marks: 2

Air flows over a spherical storage vessel of diameter 4 m at a speed of 1 m/s. To find the drag force on the vessel, a test run is to be carried out in water using a sphere of diameter 100 mm. The density and dynamic viscosity of air are 1.2 kg/m3 and 1.8 ×10-5 Pa.s, respectively. The density and dynamic viscosity of water are 1000 kg/m3 and 10-3 Pa.s, respectively. The drag force on the model is 4 N under dynamically similar conditions. The drag force (in N) on the prototype is approximately

  • A. 0.25
  • B. 0.93
  • C. 1.08
  • D. 4

Answer: C. 1.08

Question 258

Year: 2012 | Marks: 2

The velocity of an air stream is 20 m/s. The densities of mercury and air are 13600 kg/m3 and 1.2 kg/m3, respectively. The gravitational acceleration may be taken as 10 m/s2. When a Pitot-static tube is placed in the stream, assuming the flow to be incompressible and frictionless, the difference between the stagnation and static pressure in the flow field (in mm Hg) would approximately be

  • A. 1760
  • B. 1.76
  • C. 0.57
  • D. 0.57 × 10–5

Answer: B. 1.76

Question 259

Year: 2012 | Marks: 2

The pressure (in bar) exerted on the bottom wall inside the vessel is approximately

Figure for question 259, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 0.238
  • B. 2.38
  • C. 23.8
  • D. 238

Answer: B. 2.38

Question 260

Year: 2012 | Marks: 2

The gate is 1 m wide perpendicular to the plane of the paper. The force (in N) exerted on the gate is approximately

Figure for question 260, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 2.23 ×103
  • B. 2.23 ×104
  • C. 2.23 ×105
  • D. 2.23 ×106 Gas (2 bar) Gate Water

Answer: C. 2.23 ×105

Question 261

Year: 2012 | Marks: 2

The power (in kW) required to propel the boat is

Figure for question 261, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 10
  • B. 20
  • C. 50
  • D. 90

Answer: B. 20

Question 262

Year: 2012 | Marks: 2

The total kinetic energy imparted to the water per second (in kW) by the pump is

Figure for question 262, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 10
  • B. 25
  • C. 28
  • D. 81

Answer: C. 28

Question 263

Year: 2012 | Marks: 2

The dimensionless velocity profile is

Figure for question 263, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 2 2 − = δ δ y y U u
  • B. 2 2 + = δ δ y y U u
  • C. 2 5.0 5.1 − = δ δ y y U u
  • D. 2 5.0 5.1 + = δ δ y y U u

Answer: A. 2 2 − = δ δ y y U u

Question 264

Year: 2012 | Marks: 2

The displacement thickness (in mm) when δ= 6 mm, is

Figure for question 264, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 2.25
  • B. 2
  • C. −2
  • D. −2.25 U y x δ (x)

Answer: B. 2

Question 265

Year: 2007 | Marks: 1

A projection manometer is to be used for measuring the dynamic pressure of an airstream ($\rho = 1.2\text{ kg/m}^3$). The least count of the manometer scale is $0.1\text{ mm}$. The manometric liquid is alcohol of specific gravity $0.8$. The lowest velocity that can be measured is (Take $g = 10\text{ m/s}^2$, $\rho_w = 1000\text{ kg/m}^3$)

  • A. $\sqrt{3}/2\text{ m/s}$
  • B. $2/\sqrt{3}\text{ m/s}$
  • C. $\sqrt{3}\text{ m/s}$
  • D. $2\text{ m/s}$

Question 266

Year: 2007 | Marks: 1

The velocity of sound

  • A. is a thermodynamic state variable
  • B. is constant for a particular fluid
  • C. depends on the velocity field for the flow
  • D. depends on whether the flow is laminar or turbulent

Question 267

Year: 2007 | Marks: 1

Consider the mass balance equation $\frac{\partial u}{\partial x} + \frac{\partial v}{\partial y} = 0$. The most appropriate set of conditions for this equation to hold good is:

  • A. steady or unsteady, and compressible or incompressible
  • B. steady or unsteady, and compressible
  • C. steady or unsteady, and incompressible
  • D. steady, and compressible or incompressible

Question 268

Year: 2007 | Marks: 1

The non-dimensional number obtained from specific heat ($c_p$), thermal conductivity ($k$) and viscosity ($\mu$) is

  • A. $\sqrt{k c_p}/\mu$
  • B. $\sqrt{k \mu}/c_p$
  • C. $k\mu/c_p$
  • D. $\mu c_p/k$

Question 269

Year: 2007 | Marks: 1

For a two-dimensional turbulent boundary layer, the wall shear stress can be expressed as $\tau_w = \mu \frac{\partial u}{\partial y}\big|_{wall}$ where $u$ is the velocity parallel to the wall and $y$ is the coordinate perpendicular to the wall. In the above expression, $\mu$ denotes

  • A. the molecular viscosity of the fluid
  • B. the turbulent eddy viscosity
  • C. an effective viscosity which is greater than the molecular viscosity
  • D. an effective viscosity that is less than the molecular viscosity

Question 270

Year: 2007 | Marks: 1

Flow-separation from a solid surface may take place if the flow is

  • A. viscous, in a positive streamwise pressure gradient
  • B. viscous, in a negative streamwise pressure gradient
  • C. inviscid, in a positive streamwise pressure gradient
  • D. inviscid, in a negative streamwise pressure gradient

Question 271

Year: 2007 | Marks: 2

It is given that a solid sphere and a hollow cube have the same outer surface area. The ratio of buoyancy force on the sphere to that on the cube, when they are fully submerged in a liquid, is given by

  • A. $\sqrt{\frac{2}{\pi}}$
  • B. $\sqrt{\frac{4}{\pi}}$
  • C. $\sqrt{\frac{6}{\pi}}$
  • D. $\sqrt{\frac{8}{\pi}}$

Question 272

Year: 2007 | Marks: 2

Given that temperature $T(x,y)$ does not change along a streamline in a steady two-dimensional, incompressible flow, the equation of the streamline is obtained from

  • A. $\frac{dy}{dx} = \frac{-(\frac{\partial T}{\partial x})}{(\frac{\partial T}{\partial y})}$
  • B. $\frac{dy}{dx} = \frac{-(\frac{\partial T}{\partial y})}{(\frac{\partial T}{\partial x})}$
  • C. $\frac{dy}{dx} = \frac{(\frac{\partial T}{\partial x})}{(\frac{\partial T}{\partial y})}$
  • D. $\frac{dy}{dx} = \frac{(\frac{\partial T}{\partial y})}{(\frac{\partial T}{\partial x})}$

Question 273

Year: 2007 | Marks: 2

Consider a two-dimensional laminar boundary layer with a constant freestream velocity. For a fluid particle very close to the wall, the signs of the material acceleration components in directions parallel and perpendicular to the solid surface are, respectively

  • A. + and -
  • B. - and +
  • C. + and +
  • D. - and -

Question 274

Year: 2007 | Marks: 2

Water enters a pipe of cross-sectional area $A_1$ that branches out into sections of equal areas $A_2$ and $A_3$ as shown in the figure below. At one instant, the flow velocities are $V_1 = 2\text{ m/s}$, $V_2 = 3\text{ m/s}$ and $V_3 = 5\text{ m/s}$. At another instant, $V_1 = 3\text{ m/s}$ and $V_2 = 4\text{ m/s}$. What is the value of $V_3$ at this instant?

Figure for question 274, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. $5\text{ m/s}$
  • B. $6\text{ m/s}$
  • C. $7\text{ m/s}$
  • D. $8\text{ m/s}$

Question 275

Year: 2007 | Marks: 2

For a two-dimensional incompressible irrotational flow, the $x$-component of velocity $u = 2x + 3y$. The corresponding $y$-component of velocity is

  • A. $2y - 3x$
  • B. $2y + 3x$
  • C. $-2y + 3x$
  • D. $-2y - 3x$

Question 276

Year: 2007 | Marks: 2

For a certain two-dimensional steady incompressible flow, the horizontal and vertical velocity components are given by $u = 6y$, $v = 0$, where $y$ is the vertical distance. The angular velocity and rate of shear strain respectively are

  • A. -3 and 3
  • B. 3 and -3
  • C. 3 and -6
  • D. -6 and 3

Question 277

Year: 2007 | Marks: 2

In a steady two-dimensional incompressible flow, the stream function ($\psi$) obeys the equation $\frac{\partial^2 \psi}{\partial x^2} + \frac{\partial^2 \psi}{\partial y^2} = 4$. A solution of this equation is

  • A. $\psi = x^2 + y^2$
  • B. $\psi = y^2 - x^2$
  • C. $\psi = xy$
  • D. $\psi = x + y$

Question 278

Year: 2007 | Marks: 2

A uniform stream of an ideal fluid with velocity $U$ and pressure $p_\infty$ flows past a circular cylinder as shown in the figure below. The fluid velocity on the cylinder wall is given by $V_\theta = 2U \sin\theta$. The pressure coefficient is defined as $C_p = \frac{p - p_\infty}{0.5\rho U^2}$. The minimum value of $C_p$ on the surface of the cylinder is

Figure for question 278, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 1
  • B. -1
  • C. -3
  • D. -4

Question 279

Year: 2007 | Marks: 2

A model of characteristic length $20\text{ cm}$ is built to study the flow of water ($\nu = 10^{-6}\text{ m}^2\text{/s}$) in an open channel of $5\text{ m}$ characteristic length. What should be the kinematic viscosity of the fluid used in the model?

  • A. $4 \times 10^{-9}\text{ m}^2\text{/s}$
  • B. $8 \times 10^{-9}\text{ m}^2\text{/s}$
  • C. $4 \times 10^{-6}\text{ m}^2\text{/s}$
  • D. $8 \times 10^{-6}\text{ m}^2\text{/s}$

Question 280

Year: 2007 | Marks: 2

Water flows steadily through a smooth circular tube of $5\text{ cm}$ diameter at a flow rate of $\pi\text{ kg/s}$. Take viscosity $\mu = 0.001\text{ Ns/m}^2$ and density $\rho = 1000\text{ kg/m}^3$. The Darcy friction factor is given as: $f_D = 64/Re_d$ for fully developed laminar flow and $f_D = 0.316 Re_d^{-0.25}$ for fully developed turbulent flow. The approximate pressure drop per unit length in the fully developed region of the tube is

  • A. $20\text{ Pa/m}$
  • B. $120\text{ Pa/m}$
  • C. $480\text{ Pa/m}$
  • D. $960\text{ Pa/m}$

Question 281

Year: 2007 | Marks: 2

Consider a constant pressure boundary layer over a flat plate of length $L = 3\text{ m}$. The freestream velocity is $U = 60\text{ m/s}$ and the density and viscosity of the fluid respectively are $\rho = 1.23\text{ kg/m}^3$ and $\mu = 1.79 \times 10^{-5}\text{ Ns/m}^2$. Transition occurs at a distance $x_{cr} = 0.1\text{ m}$ from the leading edge. If the freestream velocity is changed to $120\text{ m/s}$, $x_{cr}$ becomes

  • A. $0.2\text{ m}$
  • B. $0.1\text{ m}$
  • C. $0.05\text{ m}$
  • D. $0.005\text{ m}$

Question 282

Year: 2007 | Marks: 2

For a laminar boundary layer with constant freestream velocity (i.e. $dp/dx = 0$), the variation of $\partial u/\partial y$ with distance $y$ from the wall is given by

Figure for question 282, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. Graph A
  • B. Graph B
  • C. Graph C
  • D. Graph D

Question 283

Year: 2007 | Marks: 2

Consider the steady flow of a uniform stream past a circular cylinder, for a viscous fluid. The following two cases are compared: (I) cylinder is rotating at a slow rate about its axis (II) cylinder is not rotating. Consider the statements — P: The lift force in case I is zero; Q: The lift force in case II is zero; R: The drag force in case I is non-zero; S: The drag force in case II is zero. Which one of the following combinations is TRUE?

  • A. P, Q, R
  • B. P, R, S
  • C. P, S
  • D. Q, R

Question 284

Year: 2007 | Marks: 2

An orifice plate of $60\text{ mm}$ diameter and discharge coefficient $0.6$ is used for measuring the flow rate of air ($\rho = 1.2\text{ kg/m}^3$, $\mu = 1.8 \times 10^{-5}\text{ kg m}^{-1}\text{s}^{-1}$) through a pipe of $100\text{ mm}$ diameter. A manometer (with water as the working liquid) connected across the orifice plate reads $180\text{ mm}$. The air flow rate is approximately equal to

  • A. $0.3\text{ m}^3\text{/s}$
  • B. $0.1\text{ m}^3\text{/s}$
  • C. $0.01\text{ m}^3\text{/s}$
  • D. $0.003\text{ m}^3\text{/s}$

Question 285

Year: 2007 | Marks: 2

The velocity of an airstream ($\rho = 1.0\text{ kg/m}^3$) is to be measured using a pitot-static tube. The level difference between the two arms of the manometer is $2\text{ cm}$ of water. The velocity is

  • A. $0.02\text{ m/s}$
  • B. $2.0\text{ m/s}$
  • C. $10\text{ m/s}$
  • D. $20\text{ m/s}$

Question 286

Year: 2007 | Marks: 2

Match the items in the following columns using the most appropriate combinations: Column 1: (P) $\frac{dp}{dz} = \frac{-pg}{RT}$, (Q) Lift, (R) Stream function, (S) Compressibility. Column 2: (1) Volume flow rate, (2) Variable density atmosphere, (3) Mach Number, (4) Circulation, (5) Reynolds Number.

  • A. P-3, Q-4, R-1, S-5
  • B. P-1, Q-2, R-4, S-3
  • C. P-4, Q-5, R-2, S-3
  • D. P-2, Q-4, R-1, S-3

Question 287

Year: 2007 | Marks: 2

Common Data: A line source and a line sink, both of unit strength, are placed on the $x$-axis at $x = -1$ and $x = +1$ respectively. In terms of the Cartesian unit vectors $\mathbf{i}$ and $\mathbf{j}$, the velocity at the point $(0,1)$ is given as

  • A. $0\mathbf{i} + 0\mathbf{j}$
  • B. $\frac{1}{2\pi}\mathbf{i}$
  • C. $\frac{1}{2\pi}\mathbf{j}$
  • D. $\frac{1}{\pi}\mathbf{i}$

Question 288

Year: 2007 | Marks: 2

Common Data: A line source and a line sink, both of unit strength, are placed on the $x$-axis at $x = -1$ and $x = +1$ respectively. If the source and sink are placed in a uniform approach stream, the resulting external flow corresponds to that

  • A. of a doublet
  • B. over a circular cylinder
  • C. over a Rankine half-body
  • D. over a Rankine oval

Question 289

Year: 2007 | Marks: 2

Linked Answer Q.25 & Q.26: A motorboat is cruising in a lake (see figure below) at a uniform speed of $10\text{ m/s}$. A $180\text{ kW}$ pump sucks water at a rate $1\text{ m}^3\text{/s}$ through an inlet pipe in the front and pumps it out with a velocity of $10\text{ m/s}$ with respect to the lake, through an outlet pipe at the rear. The total drag on the boat is

Figure for question 289, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 30 kN
  • B. 20 kN
  • C. 10 kN
  • D. Zero

Question 290

Year: 2007 | Marks: 2

Linked Answer Q.25 & Q.26: A motorboat is cruising in a lake (see figure below) at a uniform speed of $10\text{ m/s}$. A $180\text{ kW}$ pump sucks water at a rate $1\text{ m}^3\text{/s}$ through an inlet pipe in the front and pumps it out with a velocity of $10\text{ m/s}$ with respect to the lake, through an outlet pipe at the rear. The power utilized for propelling the boat is

Figure for question 290, GATE XE (Engineering Sciences): Fluid Mechanics (XE-B)

  • A. 130 kW
  • B. 100 kW
  • C. 80 kW
  • D. 30 kW

Question 291

Year: 2007 | Marks: 2

Linked Answer Q.27 & Q.28: Consider a fully developed laminar flow in a pipe of radius $R$ in which $r$ and $x$ represent the radial and axial co-ordinates respectively. The axial velocity distribution is $u(r) = \left(\frac{-R^2}{4\mu}\frac{dp}{dx}\right)\left(1 - \frac{r^2}{R^2}\right)$ and the average axial velocity is $u_m = \left(\frac{-R^2}{8\mu}\frac{dp}{dx}\right)$. The magnitude of shear stress on the wall ($\tau_{wall}$) is

  • A. $\frac{32\mu}{\rho u_m R}$
  • B. $\frac{4\mu u_m}{R}$
  • C. $\frac{\mu u_m}{R}$
  • D. $-\frac{R^2}{4}\frac{d^2p}{dx^2}$

Question 292

Year: 2007 | Marks: 2

Linked Answer Q.27 & Q.28: Consider a fully developed laminar flow in a pipe of radius $R$ in which $r$ and $x$ represent the radial and axial co-ordinates respectively. The axial velocity distribution is $u(r) = \left(\frac{-R^2}{4\mu}\frac{dp}{dx}\right)\left(1 - \frac{r^2}{R^2}\right)$ and the average axial velocity is $u_m = \left(\frac{-R^2}{8\mu}\frac{dp}{dx}\right)$. The local friction factor $C_f = \frac{\tau_{wall}}{0.5\rho u_m^2}$, with $\gamma = -\frac{dp}{dx}$ is given by

  • A. $\frac{16\mu^2}{\rho R^3 \gamma}$
  • B. $\frac{24\mu^2}{\rho R^3 \gamma}$
  • C. $-\frac{R^2}{2\rho u_m^2}\frac{d^2p}{dx^2}$
  • D. $\frac{64\mu^2}{\rho R^3 \gamma}$