Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation
By: William L. Ko.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical memorandum -- 4770.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1996
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft structures; Panels; Thermal buckling; Mechanical properties; Finite element method; Hypersonic aircraft; Fiber orientation
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 97-0960-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.