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Taken together, the load cases in this topic exist to answer which question?

  • A.How fast the aircraft can fly
  • B.How much fuel the aircraft will burn
  • C.How many passengers the aircraft can carry
  • D.What load each part carries, and how often

Answer: D

Load analysis produces the numbers that stress analysis then works to: a peak value for static strength and a spectrum for fatigue, resolved separately for every part of the airframe. Everything downstream in structural design depends on getting these right.

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