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  1. 1
    Layerwise finite elements for smart piezoceramic composite plates in thermal environments

    Layerwise finite elements for smart piezoceramic composite plates in thermal environments by Lee, Ho-Jun

    [Washington, DC] : [Springfield, Va.] :; [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  2. 2
    Response of composite panels with stiffness gradients due to stiffener terminations and cutouts

    Response of composite panels with stiffness gradients due to stiffener terminations and cutouts

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  3. 3
    Analysis of static contact in laminated composite plates using damage mechanics : final technical report

    Analysis of static contact in laminated composite plates using damage mechanics : final technical report by Allen, David H., 1950-

    Hampton, VA : [Springfield, Va.] : NASA Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  4. 4
    Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data

    Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data by Taleghani, Barmac K.

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va. :] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  5. 5
    Buckling behavior of long anisotropic plates subjected to combined loads

    Buckling behavior of long anisotropic plates subjected to combined loads by Nemeth, Michael P.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  6. 6
    Novel composites for wing and fuselage applications

    Novel composites for wing and fuselage applications by Sobel, L. H.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  7. 7
    Composite structural materials : semi-annual progress report, September 30, 1984 through April 30, 1985

    Composite structural materials : semi-annual progress report, September 30, 1984 through April 30, 1985 by Loewy, Robert G.

    Troy, N.Y. : [Washington, D.C.] : [Springfield, Va.] : Rensselaer Polytechnic Institute ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


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  8. 8
    Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box

    Correlation of structural analysis and test results for the McDonnell Douglas stitched/RFI all-composite wing stub box

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  9. 9
    Ultrasonic verification of fire wave fronts in unidirectional graphite epoxy composite

    Ultrasonic verification of fire wave fronts in unidirectional graphite epoxy composite by Seng, Han-Song

    Cambridge, Mass. : [Cleveland, Ohio] : [Springfield, Va.] :; Cambridge, Mass. : [Cleveland, Ohio] : [Springfield, Va. :] : Massachusetts Institute of Technology ; National Aeronautics and Space Administration, Lewis Research Center ; [For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  10. 10
    An acoustic emission and acousto-ultrasonic analysis of impact damaged composite pressure vessels

    An acoustic emission and acousto-ultrasonic analysis of impact damaged composite pressure vessels by Walker, James L.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  11. 11
    Global/local stress analysis of composite panels

    Global/local stress analysis of composite panels by Ransom, Jonathan B.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1989
    Format: Government Document Book


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  12. 12
    Experimental spin testing of integrally damped composite plates : final report on a research project funded through NASA research grant number NCC3-493

    Experimental spin testing of integrally damped composite plates : final report on a research project funded through NASA research grant number NCC3-493 by Kosmatka, J. B. (John B.)

    La Jolla, Calif. : [Washington, DC] : [Springfield, Va.] : Division of Structural Engineering, University of California, San Diego ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


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  13. 13
    Structural durability of damaged metallic panel repaired with composite patches

    Structural durability of damaged metallic panel repaired with composite patches by Minnetyan, Levon

    [Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1997
    Format: Government Document Book


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  14. 14
    Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box

    Analysis of selected compression splice joint locations in a graphite-epoxy transport wing stub box by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  15. 15
    Load transfer in the stiffener-to-skin joints of a pressurized fuselage : NASA grant NAG-1-537, performance period, November 1, 1991 to April 30, 1995

    Load transfer in the stiffener-to-skin joints of a pressurized fuselage : NASA grant NAG-1-537, performance period, November 1, 1991 to April 30, 1995 by Johnson, Eric R.

    Blacksburg, Va. : [Washington, D.C. : National Aeronautics and Space Administration] ; [Springfield, Va. : National Technical Information Service], College of Engineering, Virginia Polytechnic Institute and State University ; 1995
    Format: Government Document Book


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  16. 16
    Analytical study of graphite-epoxy tube response to thermal loads

    Analytical study of graphite-epoxy tube response to thermal loads by Knott, Tamara W.

    Blacksburg, Va. : [Washington, D.C.] : [Springfield, Va.] : College of Engineering, Virginia Polytechnic Institute and State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


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  17. 17
    Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading

    Strength of graphite/epoxy bolted wing-skin splice specimens subjected to outdoor exposure under constant load and yearly fatigue loading by Wichorek, Gregory R.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986
    Format: Government Document Book


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  18. 18
    Test report--fault current through graphite filament reinforced plastic : under contract NAS8-39983

    Test report--fault current through graphite filament reinforced plastic : under contract NAS8-39983 by Evans, R. W.

    Marshall Space Flight Center, Ala. : [Springfield, Va.] : National Aeronautics and Space Administration, [George C. Marshall Space Flight Center] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


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  19. 19
    Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data

    Finite-element vibration analysis and modal testing of graphite epoxy tubes and correlation between the data by Taleghani, Barmac K.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


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  20. 20
    Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections

    Static and free-vibrational response of semi-circular graphite-epoxy frames with thin-walled open sections by Collins, J. Scott, 1964-

    Blacksburg, Va. :; Blacksburg, Va. : College of Engineering, Virginia Polytechnic Institute and State University, 1989
    Format: Government Document Book


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