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This section includes 13 Mcqs, each offering curated multiple-choice questions to sharpen your Thermodynamics knowledge and support exam preparation. Choose a topic below to get started.
1. |
Rayleigh line represents the locus of states with same impulse pressure and mass velocity. |
A. | true |
B. | false |
Answer» B. false | |
2. |
The impulse pressure(I) is given by |
A. | F/A |
B. | p + (density)(V2) |
C. | p + (G2)/(density) |
D. | all of the mentioned |
Answer» E. | |
3. |
Normal shocks can be treated as shock waves parallel to the flow.a) trueb) false 3.Within the mean free path of molecule, flow passes from |
A. | trueb) false 3.Within the mean free path of molecule, flow passes froma) supersonic state |
B. | false 3.Within the mean free path of molecule, flow passes froma) supersonic stateb) subsonic state |
C. | subsonic to supersonic state |
D. | supersonic to subsonic stateView Answer |
Answer» C. subsonic to supersonic state | |
4. |
RAYLEIGH_LINE_REPRESENTS_THE_LOCUS_OF_STATES_WITH_SAME_IMPULSE_PRESSURE_AND_MASS_VELOCITY.?$ |
A. | true |
B. | false |
Answer» B. false | |
5. |
The impulse pressure(I) is given b? |
A. | F/A |
B. | p + (density)(V<sup>2</sup>) |
C. | p + (G<sup>2</sup>)/(density) |
D. | all of the mentioned |
Answer» E. | |
6. |
Which of the following is true about adiabatic flow in constant area duct with friction? |
A. | it has constant G |
B. | it has constant ho |
C. | it follows Fanno line |
D. | all of the mentioned |
Answer» E. | |
7. |
The end states of normal shock must ____ Fanno line. |
A. | lie below |
B. | lie above |
C. | lie on |
D. | none of the mentioned |
Answer» D. none of the mentioned | |
8. |
Fanno line represents the locus of points with same mass velocity and stagnation enthalpy. |
A. | true |
B. | false |
Answer» B. false | |
9. |
The impulse function is given by |
A. | F = p*A + (density)*A*(V<sup>2</sup>) |
B. | F = p*A + (density)*A*V |
C. | F = p*A + (density)*A*sqrt(V) |
D. | none of the mentioned |
Answer» B. F = p*A + (density)*A*V | |
10. |
When flow passes from supersonic to subsonic state, |
A. | pressure increases |
B. | velocity decreases |
C. | both of the mentioned |
D. | all of the mentioned |
Answer» D. all of the mentioned | |
11. |
Within the mean free path of molecule, flow passes from |
A. | supersonic state |
B. | subsonic state |
C. | subsonic to supersonic state |
D. | supersonic to subsonic state |
Answer» E. | |
12. |
Normal shocks can be treated as shock waves parallel to the flow. |
A. | true |
B. | false |
Answer» C. | |
13. |
Shock waves are highly localized irreversiblities in flow. |
A. | true |
B. | false |
Answer» B. false | |