Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels

Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.

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Bibliographic Details
Online Access:	Click here to view memorandum online
Main Author:	Ko, William L.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Jackson, Raymond H.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [National Technical Information Service, distributor], 1991.
Series:	NASA technical memorandum ; 4290.
Subjects:	Aircraft structures. Aspect ratio. Buckling. Combined stress. Compressive strength. Honeycomb cores. Hypersonic vehicles. Panels. Rayleigh-Ritz method. Sandwich structures. Shear strength. Structural analysis.

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Norlin Library - Government Information - Microform

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Call Number:	NAS 1.15:4290
NAS 1.15:4290	Restricted Place a Hold

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Call Number:	NAS 1.15:4290
NAS 1.15:4290	Available