The Resource Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods, William L. Ko, (microform)

Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods, William L. Ko, (microform)

Label
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods
Title
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods
Statement of responsibility
William L. Ko
Creator
Contributor
Subject
Language
eng
Additional physical form
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.
Cataloging source
GPO
http://library.link/vocab/creatorName
Ko, William L
Government publication
federal national government publication
Index
no index present
Literary form
non fiction
http://library.link/vocab/relatedWorkOrContributorName
NASA Dryden Flight Research Center
Series statement
NASA technical memorandum
Series volume
4643
http://library.link/vocab/subjectName
  • Aerodynamic heating
  • Aerodynamic loads
  • Aircraft design
  • Applications programs (Computers)
  • Aspect ratio
  • Computer-aided design
  • Critical temperature
  • Energy methods
  • Finite element method
  • Hypersonic planes
  • Rayleigh-Ritz method
  • Rectangular panels
  • Sandwich structures
  • Thermal buckling
Label
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods, William L. Ko, (microform)
Link
http://purl.access.gpo.gov/GPO/LPS60789
Instantiates
Publication
Note
  • "NASA Dryden Flight Research Center."
  • Available online
Control code
ocm60694605
Extent
1 v.
Form of item
microfiche
Reproduction note
Microfiche.
Stock number
N96-15641
System control number
(Sirsi) 1370239
Label
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods, William L. Ko, (microform)
Link
http://purl.access.gpo.gov/GPO/LPS60789
Publication
Note
  • "NASA Dryden Flight Research Center."
  • Available online
Control code
ocm60694605
Extent
1 v.
Form of item
microfiche
Reproduction note
Microfiche.
Stock number
N96-15641
System control number
(Sirsi) 1370239

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