1 option
Compression response of a sandwich fuselage keel panel with and without damage / David M. McGowan and Damodar R. Ambur.
- Format:
- Book
- Government document
- Author/Creator:
- McGowan, David M., author.
- Ambur, Damodar R., author.
- Series:
- NASA technical memorandum ; 110302.
- NASA technical memorandum ; 110302
- Language:
- English
- Subjects (All):
- Finite element method.
- Genre:
- Online resources.
- Physical Description:
- 1 online resource (33 pages) : illustrations
- Place of Publication:
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
- Notes:
- "February 1997."
- "Performing organization: NASA Langley Research Center"--Report documentation page
- Includes bibliographical references (pages 13-14).
- Online resource; title from PDF title page (NASA, viewed February 23, 2017).
- Other Format:
- Print version: McGowan David M. Compression response of a sandwich fuselage keel panel with and without damage
- Microfiche version: McGowan David M. Compression response of a sandwich fuselage keel panel with and without damage
- OCLC:
- 973554536
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