Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure /

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Bibliographic Details
Author / Creator:Rouse, Marshall.
Imprint:Hampton, Va. : Langley Research Center ; [Springfield, Va. :] : [National Technical Information Service, distributor], [1997]
Description:18 pages : illustrations.
Language:English
Series:NASA technical memorandum ; 110309
NASA technical memorandum ; 110309.
Subject:
Format: E-Resource Microform U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6522539
Hidden Bibliographic Details
Other authors / contributors:Langley Research Center.
Notes:Cover title.
"February 1997."
Includes bibliographical references (page 8).
Available via Internet from the NASA Web site. Address as of 9/09/04: http://techreports.larc.nasa.gov/ltrs/PDF/1997/tm/NASA-97-tm110309.pdf; current access available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:110309

MARC

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650 0 |a Composite materials  |x Research. 
650 0 |a Airplanes  |x Fuselage  |x Testing. 
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