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Aircraft Performance: Atmosphere and Air Data Measurement Practice Test
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Atmosphere and Air Data Measurement topics include: Atmosphere characteristics, air vertical development, standard atmospheric model, air data and height measurement, airflow characteristics and airspeed measurements, air data computers, mach number and air temperature measurements. Here are some common methods and parameters used to measure and analyze air: Temperature: A thermometer can be used to measure temperature, such as a mercury-in-glass thermometer or a digital thermometer. Pressure: A barometer can be used to measure atmospheric pressure. There are three basic types of... Show more
Aircraft Performance: Atmosphere and Air Data Measurement Practice Test
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25 Questions

1. What is the mach number of aircraft flying in air where the pressure ratio is 1.893?
2. ADD stands for ____________
3. QNH is a sea-level pressure which is used to measure the height above sea level.
4. Calculate the ideal temperature rise when total temperature is 440K and temperature at that point is 369K.
5. The altitude range of thermosphere is ___________
6. What is meant by indicated altitude?
7. The atmosphere is mainly divided into _______ layers.
8. Which of the following is the correct relation for mach number?
9. Dynamic pressure is directly proportional to the flow speed.
10. Which of the following is the general equation that relates flow temperature to true airspeed?
11. The altitude range of stratosphere is ___________
12. What is the relation between recovery factor and temperature?
13. The altitude range of exosphere is ________
14. Which of the following are measured by Pitot - static system in air data system?
15. Dynamic pressure is the difference between stagnation pressure and static pressure.
16. CAS stands for __________
17. International Standard Atmosphere is based on the assumption that air is a perfect gas and obeys gas law.
18. What is the relation between equivalent air speed and pressure ratio?
19. What is the hydrostatic equation?
20. The altitude range of troposphere is ___________
21. Mach number of an aircraft is affected by the shock waves created at the vortex of the aircraft.
22. Which of the following is the correct isentropic relation between pressure and temperature?
23. Pitot-static system is a primary flight instrument.
24. What are the percentages of nitrogen, oxygen, argon and carbon dioxide in atmosphere?
25. According to ISA atmospheric model what is the value of datum atmospheric temperature?