Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels
By: William L. Ko and Raymond H. Jackson.
Contributors: Jackson, Raymond H.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4290.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; National Technical Information Service, distributor]
Published: 1991
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft structures.; Aspect ratio.; Buckling.; Combined stress.; Compressive strength.; Honeycomb cores.; Hypersonic vehicles.; Panels.; Rayleigh-Ritz method.; Sandwich structures.; Shear strength.; Structural analysis.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.