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Aircraft Design Practice Test: Propulsion
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Propulsion topics include: Jet-engine thrust considerations, turbojet installed thrust, installed-thrust methodology, piston-engine and turboprop performance. Aircraft propulsion systems generally consist of an engine and a means to generate thrust, such as a propeller or nozzle. The propulsion system's thrust must balance the airplane's drag when cruising.  Here are some types of aircraft engines: Turbojet: A jet engine that uses a turbine-driven compressor to compress air for fuel combustion. The engine produces thrust by spraying a high-energy gas stream from the exhaust... Show more
Aircraft Design Practice Test: Propulsion
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25 Questions

1. Thrust generated by an engine is proportional to mass flow rate.
2. An engine has gross thrust of 150KN. If mentioned designed condition needs to be met is that the ram drag should not exceed more than 18KN then, find the net thrust by engine.
3. If manufacturer’s thrust loss requirement is 3% and engine has mass flow of 20 unit then, determine how much bleed mass flow can be used?
4. Engine manufacturer has provided the reference value of inlet pressure recovery as 0.94. If actual pressure recovery is found to be 0.91 then, find the thrust loss. Consider C of 1.25.
5. Supercharger is used to improve __________
6. Uninstalled engine data is available from __________
7. A manufacturer’s uninstalled engine is required to operate at 1.8M. Find the reference pressure recovery based on military standard.
8. At low subsonic speed, we should select _________
9. Inflow ratio is defined as __________
10. What is the limitation of current engine design?
11. A propeller is rotating with 20 rps has diameter of 2.5m. Calculate thrust produced by the propeller if thrust coefficient is 0.01.
12. Propulsive efficiency is defined as _____________
13. What do you mean by overall pressure ratio?
14. Which of the following is correct?
15. Mass flow rate will be affected by __________
16. What do you mean by installed engine thrust?
17. Find the acceptable value of ram drag if Turbojet is designed to provide net thrust of 88% of gross thrust. Engine gross thrust is 12.5KN.
18. Net thrust is given by ________
19. Determine the required thrust coefficient to produce thrust of 1000N. Given diameter is 1.2m and n=22 rps.
20. If a propeller has speed of 600 rpm and diameter of 1.2m and velocity of 10m/s. Find advance ratio.
21. If slip function of propeller is 0.075 and diameter is 20 ft. then, determine the velocity of propeller. Given n = 25 rps.
22. Determine thrust of propeller if propeller efficiency is 85%. Propeller is assumed to be operated with 1200 bhp and 350ft/s of velocity.
23. Fudge factor is used to obtain ______________
24. If a propeller has bhp of 700 and diameter as 1.2 ft. and rotating with 20 rps then, determine power coefficient. Consider sea level density.
25. A piston engine has bhp of 600 at sea level. Now, if engine is operating at an altitude where density ratio is 0.816 then, find the value bhp at that altitude.