 
			 
			MCQOPTIONS
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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 | |