Impact damage tolerance of composite repairs to highly-loaded, high temperature composite structures (original) (raw)

Composites Part A: Applied Science and Manufacturing, 2011

Abstract

In substantiating the strength of highly-loaded composite structure for aerospace application, consideration must be given to the effect of in-service damage on the residual strength. The same consideration is not given to repaired structure, which may be non-conservative, especially if the aircraft were to have a repair installed early on in the life of type. The current study aims to

Alex Harman hasn't uploaded this paper.

Let Alex know you want this paper to be uploaded.

Ask for this paper to be uploaded.