MCQOPTIONS
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MCQOPTIONS
This section includes 10 Mcqs, each offering curated multiple-choice questions to sharpen your Aircraft Performance knowledge and support exam preparation. Choose a topic below to get started.
| 1. |
What is the value of n exponential in the fuel flow law for a high bypass ratio turbofan? |
| A. | 0.4 |
| B. | 0.5 |
| C. | 0.6 |
| D. | 0.7 |
| Answer» D. 0.7 | |
| 2. |
What is the velocity of maximum specific endurance of the engine when the maximum air speed is 400m/s and the exponential value is 0.2? |
| A. | 350.43 |
| B. | 490.34 |
| C. | 494.37 |
| D. | 380.43 |
| Answer» E. | |
| 3. |
What is the velocity of maximum specific air range of the engine when the maximum air speed is 400m/s and the exponential value is 0.2? |
| A. | 300.84 |
| B. | 380.43 |
| C. | 440.76 |
| D. | 494.37 |
| Answer» E. | |
| 4. |
The formula for velocity of maximum specific endurance is _______________ |
| A. | ( big[ frac{3+n}{1+n} big]^{ frac{1}{4}} )V<sub>md</sub> |
| B. | ( big[ frac{2+n}{1+n} big]^{ frac{1}{4}} )V<sub>md</sub> |
| C. | ( big[ frac{2+n}{2-n} big]^{ frac{1}{4}} )V<sub>md</sub> |
| D. | ( big[ frac{2-n}{2+n} big]^{ frac{1}{4}} )V<sub>md</sub> |
| Answer» E. | |
| 5. |
The formula for velocity of maximum specific air range is __________ |
| A. | ( big[ frac{3-n}{1+n} big]^{ frac{1}{4}} ) |
| B. | ( big[ frac{3-n}{1+n} big]^{ frac{1}{3}} )V<sub>md</sub> |
| C. | ( big[ frac{3-n}{1+n} big]^{ frac{1}{4}} )V<sub>md</sub> |
| D. | ( big[ frac{3+n}{1+n} big]^{ frac{1}{4}} )V<sub>md</sub> |
| Answer» D. ( big[ frac{3+n}{1+n} big]^{ frac{1}{4}} )V<sub>md</sub> | |
| 6. |
The value of n in fuel flow formula C=C2 ( theta^{ frac{1}{2}} )Mn is 0.2 for turbofan. |
| A. | True |
| B. | False |
| Answer» C. | |
| 7. |
The value of n in fuel flow formula C=C2 ( theta^{ frac{1}{2}} )Mn is 0.6 for turbojet. |
| A. | True |
| B. | False |
| Answer» C. | |
| 8. |
Thrust produced is the functional form of engine speed and flight Mach number. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 9. |
Which of the following is a correct form of fuel flow? |
| A. | C=C<sub>2</sub> M<sup>n</sup> |
| B. | C=C<sub>2</sub> <sup> ( frac{1}{2} )</sup>M |
| C. | C=C<sub>2</sub> M |
| D. | C=C<sub>2</sub> <sup> ( frac{1}{2} )</sup>M<sup>n</sup> |
| Answer» E. | |
| 10. |
The range and endurance are proportional to which of the following factors? |
| A. | fuel flow |
| B. | net thrust |
| C. | bypass ratio |
| D. | airspeed |
| Answer» C. bypass ratio | |