Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Program. - Contributor
Publication
1992 - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18055695M
Alternate Titles
- Study of compression loaded and impact damaged ....
Subjects
Series Statement
- NASA technical paper -- 3264.
Other Editions
- Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels
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