Research Catalog

Compression response of a sandwich fuselage keel panel with and without damage

Title
Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.
Author
McGowan David M.
Publication
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]

Details

Additional Authors
  • Ambur, Damodar R.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 110302
Subject
  • Sandwich structures
  • Graphite-epoxy composites
  • Composite structures
  • Finite element method
  • Fuselages
  • Honeycomb cores
  • Impact damage
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 97-0681-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:110302
OCLC
marcive37496094
Author
McGowan David M.
Title
Compression response of a sandwich fuselage keel panel with and without damage [microform] / David M. McGowan and Damodar R. Ambur.
Imprint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
Series
NASA technical memorandum ; 110302
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
Ambur, Damodar R.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:110302
Research Call Number
READEX Microfiche NAS 1.15:110302
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