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:	Composite materials -- Research. Airplanes -- Fuselage -- Testing. Airframes -- Design and construction.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6522539

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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

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