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Which consequence prevails when high temperature weakens epoxy bonds in composite wing structures?

A)Material creep increases non-linearly
B)Reynold's number rapidly decreases
C)Capillary action becomes dominant effect
D)Adiabatic flame compression occurs locally

💡 Explanation

Increased temperature excites constituent molecules which will then weaken, decreasing strength. Material creep increases, because these epoxy bonds yield under sustained stress due to increased temperature. Therefore the material deforms at a faster rate, rather than Reynolds number changing.

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