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Damage Tolerance of Fiber-Metal Laminates by gang qi is a document available to read on EtoBox.

This document discusses a research project analyzing the damage tolerance and durability of fiber-metal laminates (FMLs) like GLARE for aircraft structures. The project aims to develop analytical methods validated by experiments to understand the residual strength, impact behavior, post-impact fatigue, and fatigue crack growth in GLARE laminates. Numerical models are being used to simulate impact damage in GLARE and validate experimental results. The materials being tested are GLARE 4 and GLARE 5 laminates

Author
gang qi
Language
EN