Showing 1 - 15 results of 15 for search 'Goree, J. G.', query time: 0.06s Refine Results
  1. 1
    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites

    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites by Goree, J. G.

    Clemson, S.C. : [Washington, D.C. : Springfield, Va. : Dept. of Mechanical Engineering, Clemson University ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1991
    Format: Government Document Book


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  2. 2
    Shear-lag analysis of notched laminates with interlaminar debonding

    Shear-lag analysis of notched laminates with interlaminar debonding by Goree, J. G.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1984
    Format: Government Document Book


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  3. 3
    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites : semi-annual report

    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites : semi-annual report by Goree, J. G.

    Clemson, S.C. : [Washington, D.C.] : [Springfield, Va.] : Dept. of Mechanical Engineering, Clemson University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


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  4. 4
    Shear-lag analysis of a hybrid, unidirectional composite with fiber damage

    Shear-lag analysis of a hybrid, unidirectional composite with fiber damage by Goree, J. G.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
    Format: Government Document Book


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  5. 5
    The accuracy of approximate solutions in the analysis of fracture of composites semi-annual report NASA grant NSG-1297

    The accuracy of approximate solutions in the analysis of fracture of composites semi-annual report NASA grant NSG-1297 by Goree, J. G.

    [Washington, D.C. : National Aeronautics and Space Administration, 1985
    Format: Government Document Book


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  6. 6
    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites

    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites by Goree, J. G.

    Clemson, S.C. : [Washington, D.C.] : [Springfield, Va.] : Dept. of Mechanical Engineering, Clemson University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1991
    Format: Government Document Book


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  7. 7
    Mathematical modeling of damage in unidirectional composites

    Mathematical modeling of damage in unidirectional composites by Goree, J. G.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch; [For sale by the National Technical Information Service,], 1981
    Format: Government Document Book


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  8. 8
    Damage growth in composite laminates with interleaves

    Damage growth in composite laminates with interleaves by Goree, J. G.

    [Washington DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Center, distributor], 1987
    Format: Government Document Book


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  9. 9
    The accuracy of approximate solutions in the analysis of fracture of composites

    The accuracy of approximate solutions in the analysis of fracture of composites by Goree, J. G.

    [Washington, D.C.] : [National Aeronautics and Space Administration], 1985
    Format: Government Document Book


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  10. 10
    Fracture behavior of unidirectional boron/aluminum composite laminates

    Fracture behavior of unidirectional boron/aluminum composite laminates by Goree, J. G.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch; [For sale by the National Technical Information Service,], 1983
    Format: Government Document Book


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  11. 11
    Damage growth in composite laminates with interleaves

    Damage growth in composite laminates with interleaves by Goree, J. G.

    [Washington DC : Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Center, distributor, 1987
    Format: Government Document Book


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  12. 12
    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites semi-annual report

    Micro-mechanical analysis of damage growth and fracture in discontinuous fiber reinforced metal matrix composites semi-annual report by Goree, J. G.

    Clemson, S.C. : [Washington, D.C. : [Springfield, Va. : Dept. of Mechanical Engineering, Clemson University ; National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1990
    Format: Government Document Book


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  13. 13
    Preliminary investigation of crack arrest in composite laminates containing buffer strips

    Preliminary investigation of crack arrest in composite laminates containing buffer strips by Goree, J. G.

    Washington : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1978
    Format: Government Document Book


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  14. 14
    A new look at numerical analyses of free-edge stresses in composite laminates

    A new look at numerical analyses of free-edge stresses in composite laminates by Raju, I. S.

    Washington, D.C. : [Springfield, Va.] :; Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service],; National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
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    Format: Government Document Book


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  15. 15
    Opening of an interface flaw in a layered elastic half-plane under compressive loading

    Opening of an interface flaw in a layered elastic half-plane under compressive loading by Kennedy, John M.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1984
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    Format: Government Document Book


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