Combined effect of matrix cracking and stress-free edge on delamination
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Author
Contributions
- O'Brien, T. Kevin. - Contributor
- Langley Research Center. - Contributor
- United States. Army Aviation Systems Command. - Contributor
Publication
1990 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia
Language
English
Word Count
16,000 words, Guess
Page Count
64 pages
Identifiers
- OCLC Control Number25053261
- Open LibraryOL17630453M
Subjects
Series Statement
- NASA technical memorandum -- 102591.
- AVSCOM technical memorandum -- 90-B-002.
Links
Other Editions
- Combined effect of matrix cracking and stress-free edge on delamination
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