William L. Ko

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

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Author

William L. Ko

Contributions

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program. - Contributor

Publication

1996 - National Technical Information Service, distributor], Washington, DC, District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

OCLC Control Number37958339
Open LibraryOL17516413M

Subjects

Topics

PanelsThermal bucklingFiber orientation Aircraft structures Hypersonic aircraft Finite element method Mechanical properties

Series Statement

NASA technical memorandum -- 4770.

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