Showing 1 - 14 results of 14 for search 'Harris, Charles E., 1950-', query time: 0.06s Refine Results
  1. 1
    A practical engineering approach to predicting fatigue crack growth in riveted lap joints

    A practical engineering approach to predicting fatigue crack growth in riveted lap joints by Harris, Charles E., 1950-

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 2000
    Format: Government Document Book


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  2. 2
    An assessment of the state-of-the-art in the design and manufacturing of large composite structures for aerospace vehicles

    An assessment of the state-of-the-art in the design and manufacturing of large composite structures for aerospace vehicles by Harris, Charles E., 1950-

    Hampton, Va. : Hanover, MD :; Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2001
    Format: Government Document Book


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  3. 3
    A micromechanics model of the stiffness and strength of laminates with fiber waviness

    A micromechanics model of the stiffness and strength of laminates with fiber waviness by Harris, Charles E., 1950-

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1988
    Format: Government Document Book


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  4. 4
    Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures

    Development of advanced structural analysis methodologies for predicting widespread fatigue damage in aircraft structures by Harris, Charles E., 1950-

    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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  5. 5
    A micromechanics model of the stiffness and strength of laminates with fiber waviness

    A micromechanics model of the stiffness and strength of laminates with fiber waviness by Harris, Charles E., 1950-

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1988
    Format: Government Document Book


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  6. 6
    A review of nonlinear constitutive models for metals

    A review of nonlinear constitutive models for metals by Allen, David H., 1950-

    Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1990
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Book


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  7. 7
    The second joint NASA/FAA/DoD conference on aging aircraft

    The second joint NASA/FAA/DoD conference on aging aircraft

    Hampton, Va. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service [distributor], 1999
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Conference Proceeding Book


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  8. 8
    The second joint NASA/FAA/DoD conference on aging aircraft

    The second joint NASA/FAA/DoD conference on aging aircraft

    Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service [distributor, 1999
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Conference Proceeding Book


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  9. 9
    Implementation plan for the NASA Center of Excellence for Structures and Materials

    Implementation plan for the NASA Center of Excellence for Structures and Materials

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1998
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Book


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  10. 10
    FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance

    FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance

    [Hampton, Va.] : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1994
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Conference Proceeding Book


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  11. 11
    Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure

    Analytical methodology for predicting the onset of widespread fatigue damage in fuselage structure

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Book


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  12. 12
    A progressive damage methodology for residual strength predictions of notched composite panels

    A progressive damage methodology for residual strength predictions of notched composite panels by Coats, Timothy W.

    Hampton, Va. : Springfield, VA :; Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1998
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Book


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  13. 13
    Surface crack analysis applied to impact damage in a thick graphite/epoxy composite

    Surface crack analysis applied to impact damage in a thick graphite/epoxy composite by Poe, C. C.

    Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1988
    Other Authors: “…Harris, Charles E., 1950-…”
    Format: Government Document Book


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  14. 14
    A procedure for utilization of a damage-dependent constitutive model for laminated composites

    A procedure for utilization of a damage-dependent constitutive model for laminated composites by Lo, David C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992
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    Format: Government Document Book


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