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:

MARC

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245 1 0 |a Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels  |h [microform] /  |c William L. Ko and Raymond H. Jackson. 
260 |a [Washington, DC] :  |b National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c 1991. 
300 |a 1 volume. 
336 |a text  |b txt  |2 rdacontent. 
337 |a microform  |b h  |2 rdamedia. 
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490 1 |a NASA technical memorandum ;  |v 4290. 
500 |a Distributed to depository libraries in microfiche. 
533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1991]  |e 1 microfiche. 
650 7 |a Aircraft structures.  |2 nasat. 
650 7 |a Aspect ratio.  |2 nasat. 
650 7 |a Buckling.  |2 nasat. 
650 7 |a Combined stress.  |2 nasat. 
650 7 |a Compressive strength.  |2 nasat. 
650 7 |a Honeycomb cores.  |2 nasat. 
650 7 |a Hypersonic vehicles.  |2 nasat. 
650 7 |a Panels.  |2 nasat. 
650 7 |a Rayleigh-Ritz method.  |2 nasat. 
650 7 |a Sandwich structures.  |2 nasat. 
650 7 |a Shear strength.  |2 nasat. 
650 7 |a Structural analysis.  |2 nasat. 
700 1 |a Jackson, Raymond H.  |0 http://id.loc.gov/authorities/names/n81014216  |1 http://isni.org/isni/0000000067250291. 
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