Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods /

Bibliographic Details
Main Author:	Ko, William L.
Corporate Author:	NASA Dryden Flight Research Center
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Available from the National Technical Information Service], [1995]
Series:	NASA technical memorandum ; 4643.
Subjects:	Aerodynamic heating. Aerodynamic loads. Aircraft design. Applications programs (Computers) Aspect ratio. Computer aided design. Critical temperature. Energy methods. Finite element method. Hypersonic aircraft. Rayleigh-Ritz method. Rectangular panels. Sandwich structures. Thermal buckling.
Online Access:	https://purl.fdlp.gov/GPO/LPS60789

Description
Item Description:	"NASA Dryden Flight Research Center." Microform.
Physical Description:	1 volume Also available via Internet from the NASA web site. Address as of 6/21/05: http://www.nasa.gov/centers/dryden/pdf/88372main%5FH-2009.pdf; current access is available via PURL.