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Author:
Ko, William L.
Title:
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods
[microform] / William L. Ko.
Format:
[microform] /
Publisher:
National Aeronautics and Space AdministrationOffice of Management, Scientific and Technical Information Program ;
Copyright Date:
1995
Description:
1 v.
Reproduction Info:
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995]. 1 microfiche.
Subject:
Aerodynamic heating
Aerodynamic loads.
Aircraft design.
Applications programs (Computers)
Aspect ratio.
Computer-aided design
Critical temperature.
Energy methods.
Finite element method
Hypersonic planes
Rayleigh-Ritz method.
Rectangular panels.
Sandwich structures.
Thermal buckling.
Other Authors:
NASA Dryden Flight Research Center
Notes:
"NASA Dryden Flight Research Center."
Series:
NASA technical memorandum 4643
OCLC:
(OCoLC)60694605
Locations:
USUX851 --
Iowa State University - Parks Library
(Ames)
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