Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
    • 1991

  • Compressive buckling analysis of hat-stiffened panel [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
    • 1991

  • Practical theories for service life prediction of critical aerospace structural components [microform] / William L. Ko, Richard C. Monaghan, and Raymond H. Jackson.

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

  • Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Mechanical and thermal buckling analysis of sandwich panels under different edge conditions [microform] / William L. Ko.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993

  • Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating [microform] / William L. Ko.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Shear buckling analysis of a hat-stiffened panel [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Mechanical and thermal buckling analysisi of rectangular sandwich panels under different edge conditions [microform] / William L. Ko.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
    • 1994

  • Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation [microform] / William L. Ko.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
    • 1996

  • Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicle [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Anomalous buckling characteristics of laminated metal-matrix composite plates with central square holes [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side [microform] / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1997.
    • 1997

  • Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 mission [microform] / William L. Ko and Leslie Gong.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS26693

  • Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : Dryden Flight Research Center, National Aeronautics and Space Administration ; Linthicum Heights, MD : Available from NASA Center for AeroSpace Information, [1998]
    • 1998

  • Thermal behavior of a titanium honeycomb-core sandwich panel [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • Edwards, Calif. : NASA Ames Resarch Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60262

  • Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods [microform] / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60789

  • Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, VA : For sale by the National Technical Information Service], 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70454

  • Impacts of space shuttle thermal protection system tile on an F-15 aircraft vertical tail [microform] / William L. Ko.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, [1985]
    • 1985

  • Preflight transient dynamic analyses of B-52 aircraft carrying space shuttle solid rocket booster drop-test vehicle [microform] / William L. Ko and Lawrence S. Schuster.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • Large-deformation displacement transfer functions for shape predictions of highly flexible slender aerospace structures / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55847

  • Method for estimating operational loads on aerospace structures using span-wisely distributed surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, April 2013.
    • 2013-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49705

  • Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one side / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, April 1997.
    • 1997-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65665

  • Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientation / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65666

  • Curved displacement transfer functions for geometric nonlinear large deformation structure shape predictions / William L. Ko, and Van Tran Fleischer, Shun-Fat Lung.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, March 2017.
    • 2017-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo79532

  • Curvilinear displacement transfer functions for deformed shape predictions of curved structures using distributed surface strains / William L. Ko, and Van Tran Fleischer, Shun-Fat Lung.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Armstrong Flight Research Center, September 2018.
    • 2018-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo111058

  • Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37308

  • First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37309

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta