Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effectsFormat: [microform] /
Author: McGowan David M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1999] This title can be found in 1 Iowa libraries.
Modal analysis of embedded passive damping materials in composite plates with different orientations final report for NASA-Dryden Flight Research Center, joint research interchange, May 1, 1997-July 24, 1998 /Format: [microform] :
Author: Kehoe, M. W.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Analysis and testing of plates with piezoelectric sensors and actuatorsFormat: [microform] /
Author: Bevan, Jeffrey S.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1998] This title can be found in 2 Iowa libraries.
Stability analysis of plates and shells a collection of papers in honor of Dr. Manuel Stein /Format: [microform] :
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1998] This title can be found in 2 Iowa libraries.
The effect of temperature dependent material nonlinearities on the response of piezoelectric composite platesFormat: [microform] /
Author: Lee, Ho-Jun.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ;
Date: [1997] This title can be found in 2 Iowa libraries.
Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects /Author: McGowan David M.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Buckling behavior of long symmetrically laminated plates subjected to shear and linearly varying axial edge loadsFormat: [microform] /
Author: Nemeth, Michael P.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Analysis of composite ablators using massively parallel computationFormat: [microform] /
Author: Shia, David.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1995] This title can be found in 2 Iowa libraries.
Applications of symbolic computation in fracture mechanics final report /Format: [microform] :
Author: Tan, Hui-Qian.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1995] This title can be found in 2 Iowa libraries.
Real time acousto-ultrasonic NDE technique for monitoring damage in ceramic composites under dynamic loadsFormat: [microform] /
Author: Tiwari, Anil.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration ;
Date: 1995] This title can be found in 2 Iowa libraries.
Completed Beltrami-Michell formulation for analyzing radially symmetrical bodiesFormat: [microform] /
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;
Date: 1994 This title can be found in 1 Iowa libraries.
Large deformation behavior of long shallow cylindrical composite panels /Author: Carper, Douglas M.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division,
Date: 1991. This title can be found in 1 Iowa libraries.
A three-node C element for analysis of laminated composite sandwich shellsFormat: [microform] /
Author: Martin, C. Wayne.
Publisher: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;
Date: 1989. This title can be found in 2 Iowa libraries.
Electromagnetic scattering by impedance structures : semiannual report /Author: Balanis, Constantine A.,
Publisher: Hampton, VA : National Aeronautics and Space Administration, Langley Research Center,
Date: [1987] This title can be found in 1 Iowa libraries.
Observation of the initiation and progression of damage in compressively loaded composite plates containing a cutoutFormat: [electronic resource] /
Author: Waas, Anthony M.
Publisher: Pasadena, Calif. : Graduate Aeronautical Laboratories, California Institute of Technology ;
Date: 1986] This title can be found in 1 Iowa libraries.
Equivalent plate analysis of aircraft wing box structures with general planform geometryFormat: [microform] /
Author: Giles, Gary L.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1986] This title can be found in 1 Iowa libraries.
The construction of airfoil pressure models by the bonded plate method achievements, current research, technology development and potential applications /Format: [microform] :
Author: Lawing, Pierce L.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center,
Date: [1985] This title can be found in 1 Iowa libraries.
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