Showing 1 - 20 results of 117 for search '', query time: 0.07s Refine Results
  1. 1
    Thermoelastic theory for the response of materials functionally graded in two directions with applications to the free-edge problem

    Thermoelastic theory for the response of materials functionally graded in two directions with applications to the free-edge problem by Aboudi, Jacob, 1935-

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


    Save to List
    Saved in:
  2. 2
    Penetration of carbon-fabric-reinforced composites by edge cracks during thermal aging

    Penetration of carbon-fabric-reinforced composites by edge cracks during thermal aging by Bowles, Kenneth J.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:
  3. 3
    A multilayered thin film insulator for harsh environments

    A multilayered thin film insulator for harsh environments

    Cleveland, Ohio : Hanover Md. :; Cleveland, Ohio : Hanover MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for AeroSpace Information, 2002
    Format: Government Document Book


    Save to List
    Saved in:
  4. 4
    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


    Save to List
    Saved in:
  5. 5
    Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs

    Structural design and analysis of a light-weight laminated composite heat sink for spaceflight PWBs by Fan, Mark S.

    Greenbelt, Md. : [Springfield, Va.] : National Aeronautics and Space Administration, Goddard Space Flight Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


    Save to List
    Saved in:
  6. 6
    Permeability testing of impacted composite laminates for use on reusable launch vehicles

    Permeability testing of impacted composite laminates for use on reusable launch vehicles by Nettles, A. T. (Alan T.)

    Marshall Space Flight Center, Ala. : Hanover, Md. :; Marshall Space Flight Center, Ala. : Hanover, MD : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; Available from NASA Center for AeroSpace Information, 2001
    Format: Government Document Book


    Save to List
    Saved in:
  7. 7
    ANISAP, a three dimensional finite element program for laminated composites subjected to mechanical loading

    ANISAP, a three dimensional finite element program for laminated composites subjected to mechanical loading by Burns, Stephen W.

    Blacksburg, Va. : [Washington, DC] : [Springfield, Va.] : Center for Composite Materials and Structures, Virginia Polytechnic Institute and State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


    Save to List
    Saved in:
  8. 8
    A new merit function for evaluating the flaw tolerance of composite laminates

    A new merit function for evaluating the flaw tolerance of composite laminates by Mikulas, Martin M.

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


    Save to List
    Saved in:
  9. 9
    Shape sensitivity analysis of flutter response of a laminated wing

    Shape sensitivity analysis of flutter response of a laminated wing by Bergen, Fred D.

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


    Save to List
    Saved in:
  10. 10
    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


    Save to List
    Saved in:
  11. 11
    Effects of delaminations on the damped dynamic characteristics of composite laminates : mechanics and experiments

    Effects of delaminations on the damped dynamic characteristics of composite laminates : mechanics and experiments by Saravanos, D. A. (Dimitris A.)

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


    Save to List
    Saved in:
  12. 12
    Improving the fatigue resistance of adhesive joints in laminated wood structures

    Improving the fatigue resistance of adhesive joints in laminated wood structures

    Washington, D.C. : [Springfield, Va.] : U.S. Dept. of Energy, Conservation and Renewable Energy, Wind/Ocean Technology Division ; [For sale by the National Technical Information Service], 1988
    Format: Government Document Book


    Save to List
    Saved in:
  13. 13
    High strain rate deformation modeling of a polymer matrix composite

    High strain rate deformation modeling of a polymer matrix composite by Goldberg, Robert K.

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Lewis Research Center ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


    Save to List
    Saved in:
  14. 14
    An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC

    An analysis of the macroscopic tensile behavior of a nonlinear nylon reinforced elastomeric composite system using MAC/GMC by Assaad, Mahmoud

    [Cleveland, Ohio] : [Springfield, Va.] : National Aeronautics and Space Administration, Glenn Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


    Save to List
    Saved in:
  15. 15
    Q3DG, a computer program for strain-energy-release rates for delamination growth in composite laminates

    Q3DG, a computer program for strain-energy-release rates for delamination growth in composite laminates by Raju, I. S.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


    Save to List
    Saved in:
  16. 16
    Develop and demonstrate manufacturing processes for fabricating graphite filament reinforced polyimide (Gr/PI) composite structural elements

    Develop and demonstrate manufacturing processes for fabricating graphite filament reinforced polyimide (Gr/PI) composite structural elements by Chase, V. A.

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


    Save to List
    Saved in:
  17. 17
    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


    Save to List
    Saved in:
  18. 18
    A higher-order theory for geometrically nonlinear analysis of composite laminates

    A higher-order theory for geometrically nonlinear analysis of composite laminates by Reddy, J. N. (Junuthula Narasimha), 1945-

    [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [National Technical Information Service, distributor], 1987
    Format: Government Document Book


    Save to List
    Saved in:
  19. 19
    Structural efficiency study of composite wing rib structures

    Structural efficiency study of composite wing rib structures by Swanson, Gary D.

    Hampton, Va. : Blacksburg, Va. : [Springfield, Va.] : Structural Mechanics Branch, National Aeronautics and Space Administration, Langley Research Center ; College of Engineering, Virginia Polytechnic Institute and State University, NASA-Virginia Tech Composites Program ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


    Save to List
    Saved in:
  20. 20
    Computational simulation of the formation and material behavior of ice

    Computational simulation of the formation and material behavior of ice by Tong, Michael T.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:

Search Tools: