 
			 
			MCQOPTIONS
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				This section includes 5 Mcqs, each offering curated multiple-choice questions to sharpen your Thermodynamics knowledge and support exam preparation. Choose a topic below to get started.
| 1. | The bypass ratio is the ratio of | 
| A. | mass flow rates of two streams | 
| B. | pressure ratio of inlet and exit | 
| C. | volume flow rate of inlet and exit | 
| D. | none of the mentioned | 
| Answer» B. pressure ratio of inlet and exit | |
| 2. | In aircraft propulsion the most widely used engine is | 
| A. | turbojet | 
| B. | turbofan | 
| C. | turboprop | 
| D. | all of the mentioned | 
| Answer» C. turboprop | |
| 3. | We cannot use regenerators and intercoolers on aircraft engines. | 
| A. | true | 
| B. | false | 
| Answer» B. false | |
| 4. | The propulsive efficiency is given by | 
| A. | work done by engine / propulsive power | 
| B. | propulsive power / work done by engine | 
| C. | energy input rate / propulsive power | 
| D. | propulsive power / energy input rate | 
| Answer» E. | |
| 5. | When flying at high altitudes, | 
| A. | air is of less density | 
| B. | air exerts less drag force on aircraft | 
| C. | both of the mentioned | 
| D. | none of the mentioned | 
| Answer» D. none of the mentioned | |