Simulating Damage Due to a Lightning Strike Event: Effects of Temperature Dependent Properties on Interlaminar DamageA multidirectional, carbon fiber-epoxy, composite panel is subjected to a simulated lightning strike, within a finite element method framework, and the effect of material properties on the failure (delamination) response is investigated through a detailed numerical study. The numerical model of the composite panel consists of individual homogenized plies with user-defined, cohesive interface elements between them. Lightning strikes are simulated as an assumed combination of excessive heat and high pressure loadings. It is observed that the initiation and propagation of lightning-induced delamination is a significant function of the temperature dependency of interfacial fracture toughness. This dependency must be defined properly in order to achieve reliable predictions of the present lightning-induced delamination in the composite panel.
Document ID
20140008860
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Ghezeljeh, Paria Naghipour (Ohio Aerospace Inst. Cleveland, OH, United States)
Pineda, Evan Jorge (NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
July 9, 2014
Publication Date
May 20, 2014
Subject Category
Air Transportation And SafetyMechanical Engineering