Search results for: Ko, William L.
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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], 1991Physical Description: 1 volume.Holdings: Loading…
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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], 1994Physical Description: 1 volume.Holdings: Loading…
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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], 1994Physical Description: 1 volume.Holdings: Loading…
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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], 1994Physical Description: 1 volume.Holdings: Loading…
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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], 1996Physical Description: 1 volume.Holdings: Loading…
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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], 1997Physical Description: 1 volume.Holdings: Loading…
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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], 1989Physical Description: 1 volume.Holdings: Loading…
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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, 1998Physical 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.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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], 1997Physical Description: 1 volume.Holdings: Loading…
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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, 1998Physical Description: 1 volume.Holdings: Loading…
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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], 1999Physical Description: 1 volume.Holdings: Loading…
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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), 2001Physical 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.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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], 1991Physical 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.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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], 1995Physical 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.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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], 1989Physical 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.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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, 1985Physical Description: 1 volume.Holdings: Loading…
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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, 1984Physical Description: 1 volume.Holdings: Loading…
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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, 2009Physical Description: 1 online resource (iv, 79 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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, 2009Physical Description: 1 online resource (v, 23 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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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, 2010Physical Description: 1 online resource (20 pages) : illustrations.Holdings: Loading…Connect to online resource - All users (Federal Depository Library Program Persistant URL)
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Related Subjects
Finite element method
Displacement
Aircraft structures
Deformation
Buckling (Mechanics)
Stress analysis
Thermal buckling
Aerodynamic heating
Space shuttles
Stress concentration
Thermal stresses
Buckling
Honeycomb cores
Hypersonic aircraft
Sandwich structures
Structural analysis
Wings
Airplanes
Flexible wings
Heat
Laminated materials
Rayleigh-Ritz method
Strain distribution
Temperature effects
Transfer functions
Transmission
Airframes
Anisotropy
Aspect ratio
B-52 aircraft