- Additional Authors
- Description
- 1 online resource (33 pages) : illustrations.
- Series Statement
- NASA technical memorandum ; 110302
- Uniform Title
- NASA technical memorandum ; 110302.
- Subject
- Note
- "February 1997."
- "Performing organization: NASA Langley Research Center"--Report documentation page.
- Bibliography (note)
- Includes bibliographical references (pages 13-14).
- Type of Report (note)
- Funding (note)
- Sponsored by the National Aeronautics and Space Administration
- Source of Description (note)
- Description based on online resource; title from PDF title page (NASA, viewed Feb. 23, 2017).
- Call Number
- GPO Internet NAS 1.15:110302
- OCLC
- marcive973554536
- Author
McGowan, David M., author.
- Title
Compression response of a sandwich fuselage keel panel with and without damage / David M. McGowan and Damodar R. Ambur.
- Publisher
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
- Type of Content
text
- Type of Medium
computer
- Type of Carrier
online resource
- Series
NASA technical memorandum ; 110302
NASA technical memorandum ; 110302.
- Bibliography
Includes bibliographical references (pages 13-14).
- Type Of Report
Technical memorandum.
- Funding
Sponsored by the National Aeronautics and Space Administration WU 538-10-11-05
- Connect to:
- Added Author
Ambur, Damodar R., author.
Langley Research Center, issuing body.
- Other Form:
Print version: McGowan David M. Compression response of a sandwich fuselage keel panel with and without damage (OCoLC)60768453
Microfiche version: McGowan David M. Compression response of a sandwich fuselage keel panel with and without damage (OCoLC)60768453
- Gpo Item No.
0830-D (online)
- Sudoc No.
NAS 1.15:110302