Probabilistic Approach to Damage Tolerance Design of Aircraft Composite Structures

Published 2006-05-01 2 authors

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Attribution

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Abstract

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The main result of the study is that the reliability of a damage-tolerable composite structure can be assessed on a quantitative basis, allowing aircraft manufacturers, operators and flight certification authorities to establish the maintenance service guidelines and estimate the reasonable inspection intervals.

Authors

K. Lin
Andrey V. Styuart

Keywords

Computer Science
Engineering
Materials Science

Citation: K. Lin, Andrey V. Styuart (2006). Probabilistic Approach to Damage Tolerance Design of Aircraft Composite Structures. Semantic Scholar ID 3541f1ba3af9457a935fd7e2b47e14d7fcdd7549. https://doi.org/10.2514/6.2006-2156 ↗