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Flashcards

Chapter 3 - Advanced Aircraft Design

Charles Gordon Aircraft Design: Fixed Wing University English 36 cards

Cards in this deck (36)

  1. 1Name the six general classifications for military aircraft.v
  2. 2List four design features of advanced trainers that differ from their ab-initio counterpart.v
  3. 3Why does the PC-9 require more advanced lift augmentation devices than the CT-4?v
  4. 4For a fighter aircraft, what handling characteristic is critical to achieving a valid targeting solution in an air-to-air engagement?v
  5. 5What factors have led to a reduction in the requirement for bombers?v
  6. 6State three design features that assist in achieving stealth capability.v
  7. 7Why are jamming systems and active countermeasures often fitted to bombers?v
  8. 8Why are maritime patrol aircraft rarely powered by turbojet engines?v
  9. 9What is the difference between the elastic region and the plastic region when considering material fatigue?v
  10. 10Describe one method by which an aircraft designer is able to mitigate against the effects of material fatigue.v
  11. 11What two aspects of flight testing have transformed a previously high risk exercise into a confirmation of predicted qualities and performance?v
  12. 12Name the conceptual model by which the aircraft’s behaviour may be described.v
  13. 13What is a dead-beat oscillation?v
  14. 14Define the term damping ratio.v
  15. 15To reduce control surface flutter, where should the centre of gravity of the surface be located?v
  16. 16Describe how aileron deflection may lead to torsional flexural flutter of the wing.v
  17. 17Name the two primary types of vibration.v
  18. 18Describe a node.v
  19. 19Of what material are windscreens and canopies generally made?v
  20. 20List five advantages offered to the aircraft designer by composite materials, or composites.v
  21. 21Which method of forming metals is typically used for undercarriage components and why?v
  22. 22What is meant by wet assembly when referring to aircraft assembly?v
  23. 23For what reason, other than stability, may an aircraft possess dihedral?v
  24. 24Why is the low-wing configuration better suited to aircraft undertaking training and/or aerobatics?v
  25. 25In terms of aircraft design, what is a canard?v
  26. 26What control functions do tailerons provide? On which RAAF aircraft would you find them?v
  27. 27What type of aspect ratio does the CT-4 possess?v
  28. 28In which configuration does a variable-sweep aircraft possess a high aspect ratio?v
  29. 29For what purpose does LEX re-attach airflow to the upper surface of the wing and fuselage?v
  30. 30How can wing tip design affect fuel consumption?v
  31. 31List three devices used to enhance the lift characteristics of the leading edge.v
  32. 32How are spoilers automatically deployed on landing and for what reason?v
  33. 33What is the purpose of the propeller?v
  34. 34List five design changes available to allow propellers to efficiently use greater engine power.v
  35. 35How does the scimitar shaped propeller allow a greater cruising speed?v
  36. 36What is the name given to the curved-style propeller blade found on the C-130J Hercules?v

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University Aircraft Design: Fixed Wing Flashcards on Chapter 3 - Advanced Aircraft Design, created by Charles Gordon on 29/11/2018.
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