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Tuesday, November 10, 2020 | History

3 edition of Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure found in the catalog.

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

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

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Published by Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Composite materials -- Research.,
  • Airplanes -- Fuselage -- Testing.,
  • Airframes -- Design and construction.

  • Edition Notes

    StatementMarshall Rouse ... [et al.].
    SeriesNASA technical memorandum -- 110309.
    ContributionsLangley Research Center.
    The Physical Object
    FormatMicroform
    Pagination18 p.
    Number of Pages18
    ID Numbers
    Open LibraryOL16114762M


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