Research Catalog

Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation

Title
Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation [microform] / William L. Ko.
Author
Ko, William L.
Publication
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.

Details

Additional Authors
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Description
1 v.
Series Statement
NASA technical memorandum ; 4770
Subject
  • Aircraft structures
  • Panels
  • Thermal buckling
  • Mechanical properties
  • Finite element method
  • Hypersonic aircraft
  • Fiber orientation
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 97-0960-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:4770
OCLC
marcive37958339
Author
Ko, William L.
Title
Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation [microform] / William L. Ko.
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
Series
NASA technical memorandum ; 4770
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:4770
Research Call Number
READEX Microfiche NAS 1.15:4770
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