Research Catalog
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Displaying 1-6 of 6 results
Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
- 1991
The buckling response of symmetrically laminated composite plates having a trapezoidal planform area [microform] / H.D. Radloff II, M.W. Hyer, M.P. Nemeth.
- Text
- Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Mechanical and thermal buckling analysisi of rectangular sandwich panels under different edge conditions [microform] / William L. Ko.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
- 1994
Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels [microform] / Navin Jaunky and Norman F. Knight, Jr., Damodar R. Ambur.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods [microform] / William L. Ko.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : Available from the National Technical Information Service, 1995]
- 1995
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS60789Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory / Michael P. Nemeth.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.
- 2014-3
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo55308
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