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Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets /

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Bibliographic Details
Main Authors: McGowan, David M. (Author), Ambur, Damodar R. (Author)
Format: Government Document eBook
Language:English
Published: Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 1997.
Series:NASA technical memorandum ; 110303.
Subjects:
Graphite-epoxy composites.
Honeycomb cores.
Impact damage.
Notch sensitivity.
Sandwich structures.
Online Access:https://purl.fdlp.gov/GPO/LPS53733
Description
Item Description:"February 1997."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (37 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 12-13).