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Aircraft Performance: Cruising Performance Practice Test
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Avg score: 68% Most missed: “Step climb helps in saving fuel.”
Cruising Performance topics include: Specific air range and endurance, aircraft range with thrust producing engines, cruise methods, fuel flow laws effect, wat effect on cruise performance and aircraft with mixed power plants. Cruise performance is a key aspect of an aircraft's capabilities. It refers to an aircraft's performance characteristics during the cruising phase of a flight. The cruising phase is an important stage for aircraft performance optimization.  Cruise performance determines an aircraft's ability to: Maintain optimal speed Maintain optimal altitude Maintain optimal fuel... Show more
Aircraft Performance: Cruising Performance Practice Test
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25 Questions

1. In cruise performance the aircraft is considered to be steady, level, straight, symmetric flight with uniform acceleration.
2. Which of the following is a reason of disadvantage of cruise method 2?
3. What is the significance of first fuel flow law?
4. The range and endurance are proportional to which of the following factors?
5. The endurance of cruise method 2 is identical to that of cruise method 1.
6. The value of ‘n’ in fuel flow formula C=C2\(\theta^{\frac{1}{2}}\)Mn is 0.2 for turbofan.
7. Minimum range is given when the aircraft is fly’s at u=1.316.
8. What is specific fuel consumption?
9. The second fuel flow law is used in the turbojet or turbofan.
10. Which of the following does range factor consists?
11. The formula for velocity of maximum specific endurance is _______________
12. What is Brequet Range expression?
13. In cruise method 1 the air pressure is decreased whereas the aircraft weight is increased.
14. The range factor of cruise method 3 is identical to that of cruise method 1.
15. Which factor must be reduced in constant angle of attack and constant altitude method?
16. What is endurance factor?
17. What is the relation between air temperature and the aircraft range?
18. What is the range of thrust producing engine?
19. Relative airspeed acts as a shaping factor.
20. Which of the following is a reason of disadvantage of cruise method 3?
21. What is meant by fuel ratio?
22. The formula for velocity of maximum specific air range is __________
23. What is the relation between altitude and the aircraft range?
24. Step climb helps in saving fuel.
25. In Cruise method 2 endurance is more concentrated than distance travelled.