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Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation / William L. Ko.
Author:
Ko, William L.
Published:
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
Physical Description:
1 online resource (v, 30 pages) : illustrations
Additional Creators:
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Access Online
purl.fdlp.gov
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Series:
NASA technical memorandum ; 4770
Restrictions on Access:
Free-to-read Unrestricted online access
Report Numbers:
NAS 1.15:4770
Subject(s):
Aircraft structures
Thermal buckling
Mechanical properties
Finite element method
Hypersonic aircraft
Note:
Title from title screen (viewed March 2, 2016).
"December 1996."
Bibliography Note:
Includes bibliographical references (page 15).
View MARC record
| catkey: 17288412