Which mechanical failure occurs when a composite aircraft wing exceeds designed flex?

💡 Explanation

Delamination occurs as excess flex induces interlaminar shear stresses causing *bond rupture* between plies; because the adhesive forces are exceeded, therefore plies separate rather than experiencing fiber failure or elastic deformation.

• Which consequence results when electron orbitals hybridize incorrectly in cytochrome oxidase?
• Which outcome during oil pipeline operation causes increased pumping costs?
• Which outcome results when a Stirling engine heat exchanger is fouled?
• Which image degradation results when partial coherence illuminates objects?
• Which effect indicates degraded fringe visibility during optical interferometry?
• Which consequence results when hydrostatic pressure overcomes bearing lubricating oil viscosity?