Compression response of a sandwich fuselage keel panel with and without damage / David M. McGowan and Damodar R. Ambur.
| Author/creator | McGowan, David M. author. |
| Other author | Ambur, Damodar R., author. |
| Other author | Langley Research Center, issuing body. |
| Format | Electronic |
| Publication | Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997. |
| Description | 1 online resource (33 pages) : illustrations. |
| Supplemental Content | https://purl.fdlp.gov/GPO/LPS72357 |
| Series | NASA technical memorandum ; 110302 NASA technical memorandum 110302. ^A467613 |
| General note | "February 1997." |
| General note | "Performing organization: NASA Langley Research Center"--Report documentation page. |
| General note | GPO Cataloging Record Distribution Program (CRDP). |
| Bibliography note | Includes bibliographical references (pages 13-14). |
| Report note | Technical memorandum. |
| Funding information | Sponsored by the National Aeronautics and Space Administration WU 538-10-11-05 |
| Source of description | Description based on online resource; title from PDF title page (NASA, viewed Feb. 23, 2017). |
| Issued in other form | Print version: McGowan David M. Compression response of a sandwich fuselage keel panel with and without damage |
| Issued in other form | Microfiche version: McGowan David M. Compression response of a sandwich fuselage keel panel with and without damage |
| GPO item number | 0830-D (online) |
| Govt. docs number | NAS 1.15:110302 |
Availability
| Library | Location | Call Number | Status | Item Actions |
|---|---|---|---|---|
| Electronic Resources | Access Content Online | ✔ Available |