Research Catalog

Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels

Title
Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.
Author
Ko, William L.
Publication
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.

Details

Additional Authors
  • Jackson, Raymond H.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Description
1 v.
Series Statement
NASA technical memorandum ; 4290
Subject
  • Aircraft structures
  • Aspect ratio
  • Buckling
  • Combined stress
  • Compressive strength
  • Honeycomb cores
  • Hypersonic vehicles
  • Panels
  • Rayleigh-Ritz method
  • Sandwich structures
  • Shear strength
  • Structural analysis
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4290
OCLC
marcive32437582
Author
Ko, William L.
Title
Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
Series
NASA technical memorandum ; 4290
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.
Added Author
Jackson, Raymond H.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4290
Research Call Number
READEX Microfiche NAS 1.15:4290
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