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Aircraft Performance: Climb and Descent Performance Practice Test
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Avg score: 0% Most missed: “The flight path gradient of descent can be increased by increasing airspeed.”
Climb and Descent Performance topics include: Climb and descent performances with mixed power plants, thrust and power producing engines, climb gradient, climb rate, minimum fuel climb, aircraft operations performance, high performance climb, wind effects on climb and descent performance. Aircraft climb and descent performance are measured in feet per minute (ft/min) and are critical factors in the safety and efficiency of flight operations.  Here is some information about aircraft climb and descent performance: Climb rate: The rate of climb is a function of two factors: excess thrust... Show more
Aircraft Performance: Climb and Descent Performance Practice Test
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25 Questions

1. The best rate of climb occurs when the excess thrust power is minimum than drag power.
2. The thrust reduction during climb leads to ____________
3. At what rate does the minimum sink rate occur in a gliding flight?
4. Thrust is directly proportional to airspeed.
5. What is the correct formula for dimensionless rate of climb?
6. The minimum sink rate is attained by flying at a relative airspeed of u/\(\sqrt[4]{3}\).
7. What is climb rate?
8. The airspeed best for rate of climb to close to that of their minimum drag speed.
9. The simple rule thumb helps in maintain good relation between rate of descent and airspeed.
10. What is the use of partial climbs?
11. What is the distance of the safeguard path?
12. By which of the methods the flight can be descended?
13. The unit of specific heat is ft/kg.
14. The flight mach number is inversely proportional to relative pressure.
15. Which of the following is the correct safe height of an aircraft?
16. The best climb gradient is attained by flying at airspeeds less than the minimum power speeds.
17. Engines with low noise signature comply with the noise regulations and provide a better performance in the climb.
18. The airspeed chosen for after take-off climb should be same as for that of minimum gradient.
19. Drag raise is avoided by maintaining constant mach number.
20. Which of the following is the formula for specific climb?
21. The flight path is unstable during __________
22. There are two ways of aircraft descend of an aircraft.
23. Wind is the relative velocity between the air mass and the ground.
24. What is the value that maintains maximum rate and minimum power speed of the aircraft?
25. What is the unit of specific fuel consumption?