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A shear panel element in a finite element model of an airframe represents

  • A.A rigid connection
  • B.A frame carrying bending
  • C.Skin carrying shear but no direct stress
  • D.A stringer carrying axial load

Answer: C

The shear panel is the direct counterpart of the idealised skin, and combining rods with shear panels reproduces the classical boom idealisation inside a finite element model. It remains common in airframe stress work for exactly that reason.

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