Fault Tree Analysis for Composite Structural Damage
Abstract
This chapter proposed a new FTA to synthesize a diversity of damage modes and damage causes of the composite structure in a systematic manner on a macroscopic level. A typical composite panel made of CFRP was selected and three importance analyses including structural importance analysis, probability importance analysis, as well as relative probability importance analysis were conducted to rank various damage causes.
Keywords
Get Reliability Based Aircraft Maintenance Optimization and Applications now with the O’Reilly learning platform.
O’Reilly members experience books, live events, courses curated by job role, and more from O’Reilly and nearly 200 top publishers.