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1
Buckling analysis of anisotropic curved panels and shells with variable curvature
by Jaunky, Navin
[Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998

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Government Document Book
2
Development of curved-plate elements for the exact buckling analysis of composite plate assemblies including transverse-shear effects
by McGowan, David M.
Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1999

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Government Document Book
3
Structural behavior of composites with progressive fracture
by Minnetyan, Levon
[Washington, D.C.] : [Springfield, Va. : NASA ; For sale by the National Technical Information Service, 1990

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Government Document Book
4
Design, optimization, and evaluation of A1-2139 compression panel with integral T-stiffeners
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 2012

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Government Document Electronic Book
5
Design and analysis of buckling-critical large-scale sandwich composite cylindrical test articles /
by Przekop, Adam
Hamton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2020

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Government Document Book
6
Buckling of an equatorial segment of a spherical shell loaded by its own weight /
by Blum, Robert E., McComb, Harvey G.
Washington, D.C. : National Aeronautics and Space Administration, 1968

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Government Document Book
7
Qualitative properties of large buckled states of spherical shells
by Shih, Ke-gang
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering, 1985

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Government Document Electronic Book
8
An integrating matrix formulation for buckling of rotating beams including the effects of concentrated masses
by Lakin, William D.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1989

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Government Document Book
9
Buckling of thin-walled circular cylinders /
by Hilburger, Mark W. (Mark William)
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2020

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Government Document Book
10
Buckling and vibration of fiber reinforced composite plates with nanofiber reinforced matrices
by Chamis, C. C. (Christos C.)
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2011

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Electronic Book
11
Design and evaluation of a foam-filled hat-stiffened panel concept for aircraft primary structural applications /
by Ambur, D. R.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995

Government Document Book
12
The dynamic aspects of thermo-elasto-viscoplastic snap-through and creep buckling phenomena /
by Riff, R.
[Cleveland, Ohio?] : [Springfield, Va.] : [National Aeronautics and Space Administration, Lewis Research Center] ; [National Technical Information Service, distributor], 1987

Government Document Book
13
Buckling analysis of anisotropic curved panels and shells with variable curvature /
by Jaunky, Navin
[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998

Government Document Book
14
Buckling of conical shell with local imperfections /
by Cooper, Paul A.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1974

Government Document Book
15
Buckling of steel containment shells /
Washington, D.C. : The Commission, 1982

Government Document Book
16
Buckling behavior of long anisotropic plates subjected to combined loads /
by Nemeth, Michael P.
[Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995

Government Document Book
17
Cabin-fuselage-wing structural design concept with engine installation.
[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994

Government Document Book
18
Buckling and postbuckling behavior of laminated composite plates with a cutout /
by Nemeth, Michael P.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996

Government Document Book
19
Progressive failure studies of composite panels with and without cutouts /
Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information, 2001

Government Document Book
20
Experimental observations and finite element analysis of the initiation of fiber microbuckling in notched composite laminates : an annual progress report /
by Guynn, Eunice Gail, 1961-
College Station, Tex. : [Washington, D.C.] : [Springfield, Va.] : Center for Mechanics of Composites, Texas A & M University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1990

Government Document Book
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