Showing 1 - 20 results of 20 for search 'Jegley, Dawn C.', query time: 0.05s Refine Results
  1. 1
    Structural test documentation and results for the McDonnell Douglas all-composite wing stub box

    Structural test documentation and results for the McDonnell Douglas all-composite wing stub box by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1997
    Format: Government Document Book


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  2. 2
    A study of the structural efficiency of fluted core graphite-epoxy panels

    A study of the structural efficiency of fluted core graphite-epoxy panels by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1990
    Format: Government Document Book


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  3. 3
    A study of the structural efficiency of fluted core graphite-epoxy panels

    A study of the structural efficiency of fluted core graphite-epoxy panels by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1990
    Format: Government Document Book


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  4. 4
    Effect of low-speed impact damage and damage location on behavior of composite panels

    Effect of low-speed impact damage and damage location on behavior of composite panels by Jegley, Dawn C.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distrbutor], 1992
    Format: Government Document Book


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  5. 5
    Test and analysis of a stitched RFI graphite-epoxy panel with a fuel access door

    Test and analysis of a stitched RFI graphite-epoxy panel with a fuel access door by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


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  6. 6
    Effect of low-speed impact damage and damage location on behavior of composite panels

    Effect of low-speed impact damage and damage location on behavior of composite panels by Jegley, Dawn C.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; National Technical Information Service, distrbutor], 1992
    Format: Government Document Book


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  7. 7
    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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  8. 8
    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders

    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


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  9. 9
    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders

    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1988
    Format: Government Document Book


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  10. 10
    Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage

    Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage by Jegley, Dawn C.

    Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1991
    Format: Government Document Book


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  11. 11
    Effect of adhesive interleaving and discontinuous plies on failure of composite laminates subject to transverse normal loads

    Effect of adhesive interleaving and discontinuous plies on failure of composite laminates subject to transverse normal loads by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1989
    Format: Government Document Book


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  12. 12
    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders

    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders by Jegley, Dawn C.

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


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  13. 13
    Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels

    Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels by Jegley, Dawn C.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  14. 14
    Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels

    Study of compression-loaded and impact-damaged structurally efficient graphite-thermoplastic trapezoidal-corrugation sandwich and semisandwich panels by Jegley, Dawn C.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; For sale by the National Technical Information Service], 1992
    Format: Government Document Book


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  15. 15
    Structural testing of a stitched/resin film infused graphite-epoxy wing box

    Structural testing of a stitched/resin film infused graphite-epoxy wing box by Jegley, Dawn C.

    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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  16. 16
    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders

    An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders by Jegley, Dawn C.

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


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  17. 17
    An analytical study of the effects of transverse shear deformation and anisotropy on the buckling of laminated cylinders

    An analytical study of the effects of transverse shear deformation and anisotropy on the buckling of laminated cylinders by Jegley, Dawn C.

    Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1987
    Format: Government Document Book


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  18. 18
    Effect of adhesive interleaving and discontinuous plies on failure of composite laminates subject to transverse normal loads

    Effect of adhesive interleaving and discontinuous plies on failure of composite laminates subject to transverse normal loads by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1989
    Format: Government Document Book


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  19. 19
    Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage

    Compression behavior of graphite-thermoplastic and graphite-epoxy panels with circular holes or impact damage by Jegley, Dawn C.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1991
    Format: Government Document Book


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  20. 20
    Testing and analysis of curved frame specimens made from a long discontinuous fiber (LDF) material

    Testing and analysis of curved frame specimens made from a long discontinuous fiber (LDF) material by Jegley, Dawn C.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1993
    Format: Government Document Book


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