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

Bibliographic Details
Main Author: Ko, William L. (Author)
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
Series:NASA technical memorandum ; 4770.
Subjects:
Aircraft structures.
Thermal buckling.
Mechanical properties.
Finite element method.
Hypersonic aircraft.
Online Access:https://purl.fdlp.gov/GPO/gpo65666
Description
Item Description:Title from title screen (viewed March 2, 2016).
"December 1996."
Physical Description:1 online resource (v, 30 pages) : illustrations.
Bibliography:Includes bibliographical references (page 15).