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

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

By William L. Ko

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Publish Date

1996

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,National Technical Information Service, distributor]

Language

eng

Pages

-