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Discrete-layer piezoelectric plate and shell models for active tip-clearance control [microform] / P.R. Heyliger, G. Ramirez, and K.C. Pei.
Text
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1994]
1994
0 resources
Numerical simulation of the nonlinear response of composite plates under combined thermal and acoustic loading [microform] : final report, for the period ended March 15, 1995 / by Chuh Mei, principal investigator, Jayashree Moorthy.
Text
Norfolk, Va. : Old Dominion University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
A refined shear deformation theory for the analysis of laminated plates [microform] / J. N. Reddy.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
1986
0 resources
Cubic zig-zag enrichment of the classical Kirchhoff kinematics for laminated and sandwich plates / Michael P. Nemeth.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
2012
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo28057Postbuckling delamination of a stiffened composite panel using finite element methods / S. Natsiavas, C.D. Babcock and W.G. Knauss.
Text
Pasadena, California : California Institute of Technology, August, 1987.
1987-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo57134Postbuckling delamination of a stiffened composite panel using finite element methods / S. Natsiavas, C.D. Babcock and W.G. Knauss.
Text
Pasadena, California : California Institute of Technology, August, 1987.
1987-8
0 resources
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