Fluid Mechanics
Fluid Properties
Marks 1Marks 2
Boundary Layer
Marks 1Marks 2Marks 5
Turbulent Flow
Marks 1Marks 2Marks 5
Fluid Kinematics
Marks 1Marks 2
1
GATE ME 2022 Set 2
MCQ (Single Correct Answer)
+1
-0.33

Consider a steady flow through a horizontal divergent channel, as shown in the figure, with the supersonic flow at the inlet. The direction of flow is from left to right.

GATE ME 2022 Set 2 Fluid Mechanics - Fluid Dynamics Question 11 English

Pressure at location B is observed to be higher than that at an upstream location A. Which among the following options can be the reason?

A
Since volume flow rate is constant, velocity at B is lower than velocity at A
B
Normal shock
C
Viscous effect
D
Boundary layer separation
2
GATE ME 2022 Set 1
MCQ (Single Correct Answer)
+1
-0.33

In the following two-dimensional momentum equation for natural convection over a surface immersed in a quiescent fluid at temperature T (g is the gravitational acceleration, β is the volumetric thermal expansion coefficient, ν is the kinematic viscosity, u and v are the velocities in x and y directions, respectively, and T is the temperature)

$\rm u \frac{\partial u}{\partial x} + v \frac{\partial u}{\partial y} = g β (T - T_∞) + \nu \frac{\partial^2 u}{\partial y^2} $

the term gβ(T - T) represent

A
Ratio of inertial force to viscous force
B
Ratio of buoyancy force to viscous force
C
Viscous force per unit mass
D
Buoyancy force per unit mass
3
GATE ME 2022 Set 1
MCQ (More than One Correct Answer)
+1
-0

The figure shows a purely convergent nozzle with a steady, inviscid compressible flow of an ideal gas with constant thermophysical properties operating under choked condition. The exit plane shown in the figure is located within the nozzle. If the inlet pressure (P0) is increased while keeping the back pressure (Pback) unchanged, which of the following statements is/are true?

GATE ME 2022 Set 1 Fluid Mechanics - Fluid Dynamics Question 14 English
A
Mass flow rate through the nozzle will remain unchanged
B
Mach number at the exit plane of the nozzle will remain unchanged at unity
C
Mass flow rate through the nozzle will increase
D
Mach number at the exit plane of the nozzle will become more than unity
4
GATE ME 2000
MCQ (Single Correct Answer)
+1
-0.3
Navier Stoke's equation represents the conservation of
A
Energy
B
Mass
C
Pressure
D
Momentum
GATE ME Subjects
Engineering Mechanics
Machine Design
Strength of Materials
Heat Transfer
Production Engineering
Industrial Engineering
Turbo Machinery
Theory of Machines
Engineering Mathematics
Fluid Mechanics
Thermodynamics
General Aptitude