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  1. 1

    Ambient temperature fatigue tests of elements of an actively cooled honeycomb sandwich structural panel by Sharpe, Ellsworth L.

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977
    Format: Government Document Book


  2. 2

    Titanium honeycomb panel testing by Richards, W. Lance

    [Washington, D.C.] : [Springfield, Va.] :; [Washington, D.C.] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


  3. 3

    High temperature be panel development by Hardesty, R.

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


  4. 4

    High capacity demonstration of honeycomb panel heat pipes by Tanzer, H. J.

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


  5. 5

    Honeycomb technology : materials, design, manufacturing, applications and testing by Bitzer, Tom

    London ; New York : Chapman & Hall, 1997
    1st ed.
    Format: Book


  6. 6

    Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems

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


  7. 7

    Compressive and shear properties of polyamide honeycomb core by Kuenzi, Edward W.

    Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, 1974
    Rev. 1974.
    Format: Government Document Book


  8. 8

    Development, fabrication and testing of honeycomb radiator condenser by Scott, G., Engle, W.

    Canoga Park, California : Atomics International, 1965
    Format: Government Document Book


  9. 9

    A modified VAPEPS method for predicting vibroacoustic response of unreinforced mass loaded honeycomb panels by McNelis, Mark E.

    [Washington, DC] : [Springfield, Va.] : NASA ; [For sale by the National Technical Information Service], 1989
    Format: Government Document Book


  10. 10

    Acoustic treatment design scaling methods. by Kraft, R. E. (Robert Eugene)

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


  11. 11

    A novel method of testing the shear strength of thick honeycomb composites by Hodge, A. J.

    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


  12. 12

    An examination of impact damage in glass/phenolic and aluminum honeycomb core composite panels by Nettles, A. T. (Alan T.)

    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, 1990
    Format: Government Document Book


  13. 13

    Experimental evaluation of honeycomb/screen configurations and short contraction section for NASA Lewis Research Center's altitude wind tunnel by Burley, Richard R.

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


  14. 14

    Ceramic honeycomb structures and the method thereof

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


  15. 15

    Reduction of turbulence in a 5" conduit using honeycombs and screens by Saxena, Vivek

    1989
    Format: Thesis Book


  16. 16

    Design date for brazed Rene ́41 honeycomb sandwich

    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


  17. 17

    Fiber composite sandwich thermostructural behavior, computational simulation by Chamis, C. C. (Christos C.)

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1986
    Format: Government Document Book


  18. 18

    Flow quality measurements in an aerodynamic model of NASA Lewis' icing research tunnel by Canacci, Victor A.

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


  19. 19

    On the use of short-length honeycombs for turbulence management by Brodjonegoro, Irsan Soemantri

    1990
    Format: Thesis Book


  20. 20

    Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems

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