The Locator -- [(author = "Ambur Damodar R")]

9 records matched your query       



Record 1
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.
Record 2
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.
Record 3
Buckling analysis of anisotropic curved panels and shells with variable curvature Format: [microform] / Author: Jaunky, Navin. Publisher: [Washington, D.C. : National Aeronautics and Space Administration ; Date: 1998]   This title can be found in 2 Iowa libraries.
Record 4
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.
Record 5
Damage-tolerance characteristics of composite fuselage sandwich structures with thick facesheets Format: [microform] / Author: McGowan, David M. Publisher: Hampton, Va. : Langley Research Center ; Date: 1997]   This title can be found in 1 Iowa libraries.
Record 6
Compression response of a sandwich fuselage keel panel with and without damage Format: [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.
Record 7
Response of composite panels with stiffness gradients due to stiffener terminations and cutouts Format: [microform] / Publisher: [Washington, D.C. : National Aeronautics and Space Administration ; Date: 1997]   This title can be found in 2 Iowa libraries.
Record 8
Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels Format: [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.
Record 9
Influence of transverse-shear and large-deformation effects on the low-speed impact response of laminated composite plates Format: [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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