William L. Ko
Identifiers
- Open LibraryOL1248451A
Top Subjects
- Finite element method (4)
- Displacement (3)
- Deformation (3)
- Cantilever beams (3)
- Buckling (Mechanics) (2)
- Stress analysis (2)
- Curved beams (2)
Books by William L. Ko
Total count: 17
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Application of finite elastic theory to the behavior of rubber-like materialsCalifornia Institute of Technology1963-01-01
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Elastic constants for superplastically formed/diffusion bonded corrugated sandwich coreNational Aeronautics and Space Administration1980-01-01
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Finite-element reentry heat-transfer analysis of space shuttle orbiterDryden Flight Research Facility1986-01-01
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Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing #h microformNational Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility1986-01-01
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Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forcesAmes Research Center1990-01-01
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Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environmentsDryden Flight Research Facility1991-01-01
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Thermal behavior of a titanium honeycomb-core sandwich panelNASA Ames Resarch Center, Dryden Flight Research Facility1991-01-01
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Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heatingNational Technical Information Service, distributor]1994-01-01
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Thermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientationNational Technical Information Service, distributor]1996-01-01
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Stress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicleNational Aeronautics and Space Administration, Dryden Flight Research Center1997-01-01
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Mechanical- and thermal-buckling behavior of rectangular plates with different central cutoutsDryden Flight Research Center, National Aeronautics and Space Administration1998-01-01
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Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite facesAvailable from NASA Center for AeroSpace Information1999-01-01
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Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 missionNational Aeronautics and Space Administration, Dryden Flight Research Center2001-01-01
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Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehiclesformulation of Ko displacement theoryNational Aeronautics and Space Administration, Dryden Flight Research Center2010-01-01
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Extension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structuresNational Aeronautics and Space Administration, Dryden Flight Research Center2011-01-01
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First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strainsNational Aeronautics and Space Administration, Dryden Flight Research Center2012-01-01
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Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strainsNational Aeronautics and Space Administration, Dryden Flight Research Center2012-01-01