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Taken together, the methods in this topic exist to determine

  • A.The aircraft's maximum speed
  • B.The wing's stalling angle
  • C.The cabin pressure differential
  • D.The wall shear flows and the shear centre

Answer: D

Shear flow analysis produces the wall-by-wall shear distribution under transverse load and torque, and locates the shear centre. Those two results size the skins and webs and feed directly into the aeroelastic behaviour of the wing.

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