Aerostructures – Properties & Performance

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Bending Stress Analysis
(a) Derive the expressions that describe the shear force and bending moment across the length of the cantilever.
(b) Applying closed-form solution, solve for the highest tensile stress experienced by the wing. Indicate clearly the location at which this maximum bending stress will occur.

Deflection Analysis
(a) By referring to solved solutions in references / textbooks, derive the expression that describes the vertical deflection
experienced across the length of the cantilever.
(b) Estimate the maximum deflection on the cantilever and indicate clearly the location at which it occur.

Structural Repair

(a) Conventional repair using solid rivets
(b) Bonded repair using structural adhesive


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