Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure
By: Marshall Rouse ... [et al.].
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 110309.
Publisher: Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 18
Subjects: Composite materials -- Research.; Airplanes -- Fuselage -- Testing.; Airframes -- Design and construction.
Notes: Cover title.

Shipping list no.: 1997-0768-M.

"February 1997."

Includes bibliographical references (p. 8).

Also 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.

Microfiche. [Washington, D.C.] : NASA ; SuptDocs/GPO, 1997. 1 microfiche : negative.