Search results for: Ko, William L.

Showing 21 - 40 results of 52 Refine Results
  1. 21

    Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [National Technical Information Service, distributor], 1991
    Physical Description: 1 volume.
    Government Document Microfilm Book
  2. 22

    Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1994
    Physical Description: 1 volume.
    Government Document Microfilm Book
  3. 23

    Shear buckling analysis of a hat-stiffened panel

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1994
    Physical Description: 1 volume.
    Government Document Microfilm Book
  4. 24

    Mechanical and thermal buckling analysisi of rectangular sandwich panels under different edge conditions

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1994
    Physical Description: 1 volume.
    Government Document Microfilm Book
  5. 25

    Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1996
    Physical Description: 1 volume.
    Government Document Microfilm Book
  6. 26

    Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center ; [National Technical Information Service, distributor], 1997
    Physical Description: 1 volume.
    Government Document Microfilm Book
  7. 27

    Effect of internal convection and internal radiation on the structural temperatures of space shuttle orbiter

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [For sale by the National Technical Information Service], 1989
    Physical Description: 1 volume.
    Government Document Microfilm Book
  8. 28

    Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts

    Authors: Ko, William L.
    Published: Dryden Flight Research Center, National Aeronautics and Space Administration ; Available from NASA Center for AeroSpace Information, 1998
    Physical Description: 1 volume., Also available via Internet from the NASA/Dryden web site. Address as of 7/31/03: http://www.dfrc.nasa.gov/DTRS/1998/PDF/H-2206.pdf; current access is available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book
  9. 29

    Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1997
    Physical Description: 1 volume.
    Government Document Microfilm Book
  10. 30

    Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holes

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center ; National Technical Information Service, distributor, 1998
    Physical Description: 1 volume.
    Government Document Microfilm Book
  11. 31

    Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center ; [National Technical Information Service, distributor], 1999
    Physical Description: 1 volume.
    Government Document Microfilm Book
  12. 32

    Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 mission

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center ; Available from NASA Center for AeroSpace Information (CASI), 2001
    Physical Description: 1 volume., Also available via Internet from the NASA web site. Address as of 2/11/03: http://www.dfrc.nasa.gov/DTRS/2001/PDF/H-2453.pdf ; current access is available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book
  13. 33

    Thermal behavior of a titanium honeycomb-core sandwich panel

    Authors: Ko, William L.
    Published: NASA Ames Research Center, Dryden Flight Research Facility ; [National Technical Information Service, distributor], 1991
    Physical Description: 13 pages : charts ; 28 cm., Also available via Internet from the NTRS web site. Address as of 5/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910008120%5F1991008120.pdf; current access is available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book
  14. 34

    Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Available from the National Technical Information Service], 1995
    Physical Description: 1 volume., Also available via Internet from the NASA web site. Address as of 6/21/05: http://www.nasa.gov/centers/dryden/pdf/88372main%5FH-2009.pdf; current access is available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book
  15. 35

    Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989
    Physical Description: 25 pages : illustrations ; 28 cm., Also available via Internet from the NASA Technical Report Server web site. Address as of 6/6/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900003353%5F1990003353.pdf; current access available via PURL.
    Connect to online resource - All users (Federal Depository Library Program Persistant URL)
    Government Document Microfilm Book
  16. 36

    Impacts of space shuttle thermal protection system tile on an F-15 aircraft vertical tail

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1985
    Physical Description: 1 volume.
    Government Document Microfilm Book
  17. 37

    Preflight transient dynamic analyses of B-52 aircraft carrying space shuttle solid rocket booster drop-test vehicle

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984
    Physical Description: 1 volume.
    Government Document Microfilm Book
  18. 38

    Further development of Ko displacement theory for deformed shape predictions of nonuniform aerospace structures

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2009
    Physical Description: 1 online resource (iv, 79 pages) : illustrations.
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    Government Document Electronic eBook
  19. 39

    Applications of Ko displacement theory to the deformed shape predictions of the doubly-tapered Ikhana wing

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2009
    Physical Description: 1 online resource (v, 23 pages) : illustrations.
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    Government Document Electronic eBook
  20. 40

    Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles : formulation of Ko displacement theory

    Authors: Ko, William L.
    Published: National Aeronautics and Space Administration, Dryden Flight Research Center, 2010
    Physical Description: 1 online resource (20 pages) : illustrations.
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    Government Document Electronic eBook