State-of-the-Art Review on Composite Material Fatigue/ Damage Tolerance

Amory, Reginald L.; Wang, David S.

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State-of-the-Art Review on Composite Material Fatigue/ Damage Tolerance

1985-12-01
By Amory, Reginald L. ; Wang, David S.

File Language:

English

Details

Creators:

Amory, Reginald L. ; Wang, David S.
Corporate Creators:

B & M Technological Services, Inc
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. Technical Center
Subject/TRT Terms:
Publication/ Report Number:

DOT/FAA/CT-85/7
Resource Type:

Tech Report
Geographical Coverage:

United States
Edition:

Final Report
Corporate Publisher:

United States. Department of Transportation. Federal Aviation Administration. William J. Hughes Technical Center
Abstract:

A state-of-the-art review on composite material fatigue damage tolerance was conducted to investigate the literature for fatigue life prediction methodologies including stress-based methodologies, strength degradation models, and damage growth models. A critical review was made of each methodology and its commensurate basic equations of importance. Experimental data were reviewed and the behavior of specimens was correlated with that of civil aircraft components. The report also examined the six recognized methods for the non-destructive testing of fibrous composite materials and identified the most effective methods. Keywords Composite Civil Aircraft.
Format:

PDF
Funding:

DTFA03-84-C-00052
Download URL:

https://rosap.ntl.bts.gov/view/dot/92642/dot_92642_DS1.pdf
File Type:

[PDF - 3.53 MB]
Collection(s):

FAA William J. Hughes Technical Center for Advanced Aerospace
Main Document Checksum:

urn:sha-512:6b11ee09a344ba93906f6ce6d4f0d21c8f4b390586180a48db0c104781389e37492e181fa79a508ec9cd2850c02bca5bf3e8b3647db25412532fd23f181d4938

File Language:

English

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