Search results for: Ko, William L.
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1
Elastic constants for superplastically formed/diffusion bonded corrugated sandwich core
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, 1980Physical Description: 79 pages : illustrations ; 27 cm.Holdings: Loading…
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2
Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing
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], 1986Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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3
Stress concentration around a small circular hole in the HiMAT composite plate
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], 1985Physical Description: 1 volume : illustrations ; 28 cm.Holdings: Loading…
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4
Stress analysis of B-52 pylon hooks
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], 1985Physical Description: 1 volume.Holdings: Loading…
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5
Effects of forced and free convections on structural temperatures of shuttle orbiter during reentry flight
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], 1986Physical Description: 1 volume.Holdings: Loading…
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6
Finite-element reentry heat-transfer analysis of space shuttle orbiter
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1986Physical Description: 1 volume.Holdings: Loading…
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7
Buckling characteristics of hypersonic aircraft wing tubular panels
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986Physical Description: 1 volume.Holdings: Loading…
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8
Delamination stresses in semicircular laminated composite bars
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1988Physical Description: 1 volume.Holdings: Loading…
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9
Optimum element density studies for finite-element thermal analysis of hypersonic aircraft structures
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], 1990Physical Description: 1 volume.Holdings: Loading…
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10
Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces
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], 1990Physical Description: 1 volume.Holdings: Loading…
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11
Accuracies of Southwell and force/stiffness methods in the prediction of buckling strength of hypersonic aircraft wing tubular panels
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], 1987Physical Description: 1 volume.Holdings: Loading…
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12
Thermal stress analysis of space shuttle orbiter wing skin panel and thermal protection system
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], 1987Physical Description: 1 volume.Holdings: Loading…
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13
Thermal stress analysis of space orbiter subjected to reentry aerodynamic heating
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], 1987Physical Description: 1 volume.Holdings: Loading…
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14
Prediction of service life of aircraft structural components using the half-cycle method
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], 1987Physical Description: 1 volume.Holdings: Loading…
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15
Effect of element size on the solution accuracies of finite-element heat transfer and thermal stress analyses 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], 1987Physical Description: 1 volume.Holdings: Loading…
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16
Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991Physical Description: 1 volume.Holdings: Loading…
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17
Compressive buckling analysis of hat-stiffened panel
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1991Physical Description: 1 volume.Holdings: Loading…
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18
Practical theories for service life prediction of critical aerospace structural components
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [For sale by the National Technical Information Service], 1992Physical Description: 1 volume.Holdings: Loading…
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19
Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments
Authors: Ko, William L.
Published: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993Physical Description: 1 volume.Holdings: Loading…
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20
Mechanical and thermal buckling analysis of 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], 1993Physical Description: 1 volume.Holdings: Loading…
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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