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This section includes 31 Mcqs, each offering curated multiple-choice questions to sharpen your Hydraulic Machines knowledge and support exam preparation. Choose a topic below to get started.
1. |
Flow ratio is defined as Vf1/(2gH)1/2 |
A. | False |
B. | True |
Answer» C. | |
2. |
The speed ratio is defined as u/(2gH)1/2 |
A. | True |
B. | False |
Answer» B. False | |
3. |
Which among the following velocities cannot be found using the velocity triangle? |
A. | Tangential |
B. | Whirl |
C. | Relative |
D. | Parabolic |
Answer» E. | |
4. |
The velocities of the blade angles can be found out using________ |
A. | Mach number |
B. | Froude’s number |
C. | Velocity triangles |
D. | Reynolds number |
Answer» D. Reynolds number | |
5. |
Non- inertial cavitation is the one in which a bubble of fluid is forced to oscillate. |
A. | True |
B. | False |
Answer» B. False | |
6. |
In case of gas turbines and compressors, degree of reaction is ________ |
A. | Static pressure drop in rotor/ static pressure drop in stage |
B. | Static pressure drop in stage/ static pressure drop in rotor |
C. | Isentropic enthalpy drop in rotor/ isentropic enthalpy drop in stage |
D. | Static temperature drop in stage/ static temperature drop in rotor |
Answer» D. Static temperature drop in stage/ static temperature drop in rotor | |
7. |
NON-_INERTIAL_CAVITATION_IS_THE_ONE_IN_WHICH_A_BUBBLE_OF_FLUID_IS_FORCED_TO_OSCILLATE.?$ |
A. | True |
B. | False |
Answer» B. False | |
8. |
The velocities of the blade angles can be found out using________$ |
A. | Mach number |
B. | Froude’s number |
C. | Velocity triangles |
D. | Reynolds number |
Answer» D. Reynolds number | |
9. |
In a Francis turbine, degree of reaction lies between _____ |
A. | 0 and 1 |
B. | 1 and 2 |
C. | 0 and 0.5 |
D. | 0.5 and 0.1 |
Answer» B. 1 and 2 | |
10. |
_________ means the angle made by absolute velocity with the tangent on the wheel is 90 degrees and the component of whirl velocity is zero. |
A. | Axial discharge |
B. | Tangential discharge |
C. | Turbulent discharge |
D. | Radial discharge |
Answer» E. | |
11. |
Flow ratio is defined as Vf1/(2gH)1/2 |
A. | False |
B. | True |
Answer» C. | |
12. |
The speed ratio is defined as u/(2gH)1/2 |
A. | True |
B. | False |
Answer» B. False | |
13. |
When the thicknesses of vanes are to be considered in the discharge of a turbine, what will be the area under consideration? |
A. | Pi*d – n*t |
B. | Pi*d – n*n*t |
C. | Pi*d – t*t |
D. | Pi*d *d– n*t |
Answer» B. Pi*d ‚Äö√Ñ√∂‚àö√ë‚àö¬® n*n*t | |
14. |
Discharge through a reaction flow reaction turbine is given by, Q = ______ |
A. | Pi*d*b*Vf1 |
B. | Pi*d*d*b*Vf1 |
C. | Pi*d*b*b*Vf2 |
D. | Pi*b*b*Vf1 |
Answer» B. Pi*d*d*b*Vf1 | |
15. |
For an actual reaction turbine, what should be the angle beta, such that the loss of kinetic energy at the outlet is to be minimum? |
A. | 90 |
B. | 45 |
C. | 60 |
D. | 30 |
Answer» B. 45 | |
16. |
When a container containing a liquid is rotated, then due to centrifugal action, then which of these energies are changed? |
A. | Kinetic energy |
B. | Pressure energy |
C. | Potential energy |
D. | Energy due to viscous force |
Answer» C. Potential energy | |
17. |
Which of these ratios are termed to be hydraulic efficiency? |
A. | Water power to delivered power |
B. | Delivered power to input power |
C. | Power lost to power delivered |
D. | Runner power to water power |
Answer» E. | |
18. |
Which of these options are best suited for the total energy change inside the runner per unit weight? |
A. | Degree of action |
B. | Degree of reaction |
C. | Turbulence |
D. | Efficiency of turbine |
Answer» C. Turbulence | |
19. |
Degree of reaction turbine is the ratio of? |
A. | Pressure energy to total energy |
B. | Kinetic energy to total energy |
C. | Potential energy to total energy |
D. | Kinetic energy to potential energy |
Answer» B. Kinetic energy to total energy | |
20. |
Super cavitation is the use of cavitation effect to create a bubble of steam inside a liquid. |
A. | True |
B. | False |
Answer» B. False | |
21. |
The process of bubble generation leads to __________ |
A. | High temperatures |
B. | High pressures |
C. | High energy densities |
D. | High volumetric ratio |
Answer» D. High volumetric ratio | |
22. |
Hydrodynamic cavitation is due to the process of _________ |
A. | Vaporisation |
B. | Sedimentation |
C. | Filtration |
D. | Excavation |
Answer» B. Sedimentation | |
23. |
Which_among_the_following_velocities_cannot_be_found_using_the_velocity_triangle? |
A. | Tangential |
B. | Whirl |
C. | Relative |
D. | Parabolic |
Answer» E. | |
24. |
In case of gas turbines and compressors, degree of reaction is _______? |
A. | Static pressure drop in rotor/ static pressure drop in stage |
B. | Static pressure drop in stage/ static pressure drop in rotor |
C. | Isentropic enthalpy drop in rotor/ isentropic enthalpy drop in stage |
D. | Static temperature drop in stage/ static temperature drop in rotor |
Answer» D. Static temperature drop in stage/ static temperature drop in rotor | |
25. |
Voids that implode near metal surface develops a_______ |
A. | Drag force |
B. | Cyclic stress |
C. | Shock waves |
D. | Flow speed |
Answer» C. Shock waves | |
26. |
At high pressure, the voids can generate ______ |
A. | Drag force |
B. | Mass density |
C. | Shock waves |
D. | Flow speed |
Answer» D. Flow speed | |
27. |
Degree of reactions are most commonly used in________ |
A. | Turbomachinery |
B. | Pressure drag |
C. | Aerodynamics |
D. | Automobiles |
Answer» B. Pressure drag | |
28. |
Cavitation usually occurs due to the changes in ________ |
A. | Pressure |
B. | Temperature |
C. | Volume |
D. | Heat |
Answer» B. Temperature | |
29. |
Voids are created due to______ |
A. | Reaction ratio |
B. | Pressure ratio |
C. | Liquid free layers |
D. | Volumetric layers |
Answer» D. Volumetric layers | |
30. |
What is the degree of reaction denoted as? |
A. | D |
B. | R |
C. | r |
D. | d |
Answer» C. r | |
31. |
The formation of vapour cavities is called _____ |
A. | Static pressure drop |
B. | Cavitation |
C. | Isentropic expansion |
D. | Emulsion |
Answer» C. Isentropic expansion | |