Damage characteristics and residual strength of composite sandwaich panels impacted with and without compression loading presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, session no. 15--damage tolerance : Long Beach, California, April 20-23, 1998 /Format: [microform] / :
Author: McGowan David M.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Effect of curvature on the impact damage characteritiscs and residual strength of composite plates presented at 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference : Long Beach, California, April 20-23, 1998 /Format: [microform] :
Author: Ambur, Damodar R.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Buckling analysis of anisotropic curved panels and shells with variable curvatureFormat: [microform] /
Author: Jaunky, Navin.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Influence of impactor mass on the damage characteristics and failure strength of laminated composite plates presented at the 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference : Long Beach, California, April 20-23, 1998 /Format: [microform] :
Author: Ambur, Damodar R.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheetsFormat: [microform] /
Author: McGowan, David M.
Publisher: Hampton, Va. : Langley Research Center ;
Date: 1997] This title can be found in 1 Iowa libraries.
Compression response of a sandwich fuselage keel panel with and without damageFormat: [microform] /
Author: McGowan David M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 1 Iowa libraries.
Response of composite panels with stiffness gradients due to stiffener terminations and cutoutsFormat: [microform] /
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panelsFormat: [microform] /
Author: Jaunky, Navin.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1995] This title can be found in 2 Iowa libraries.
Influence of transverse-shear and large-deformation effects on the low-speed impact response of laminated composite platesFormat: [microform] /
Author: Ambur, Damodar R.
Publisher: [Springfield, Va. : National Technical Information Service, distributor, [Springfield, Va. : National Technical Information Service, distributor,
Date: 1993] This title can be found in 2 Iowa libraries.
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