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William L Ko

29 cilt bulundu.

Cilt sonuçları

Heat -- Transmission.Effect of internal convection and internal radiation on the structural temperatures of space shuttle orbiterWilliam L. Ko

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

William L. Ko · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1989

Heat -- Transmission.

Structural engineeringOpen-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite facesWilliam L. Ko

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

William L. Ko · National Technical Information Service, distributor

37 sayfa · 1999

Debonding (Materials) / Stress distribution / Curved panels / Sandwich structures / Structural engineering

HooksStress analysis of B-52 pylon hooks for carrying the X-38 drop test vehicleWilliam L. Ko

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

William L. Ko · National Technical Information Service, distributor

28 sayfa · 1997

Stress concentration / Finite element method / B-52 aircraft / Pylons / Hooks

Rectangular platesMechanical- and thermal-buckling behavior of rectangular plates with different central cutoutsWilliam L. Ko

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

William L. Ko · Dryden Flight Research Center, National Aeronautics and Space Administration

42 sayfa · 1998

Structural failure / Buckling / Buckling (Mechanics) / Perforated plates / Rectangular plates

BucklingCombined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environmentsWilliam L. Ko

Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments

William L. Ko · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

23 sayfa · 1991

Metallic composites / Buckling (Mechanics) / Sandwich structures / Metal matrix composites / Buckling

Heat transferFinite-element reentry heat-transfer analysis of space shuttle orbiterWilliam L. Ko

Finite-element reentry heat-transfer analysis of space shuttle orbiter

William L. Ko · Dryden Flight Research Facility

56 sayfa · 1986

Transmission / Space shuttles / Heat / Space shuttle orbiters / Heat transfer

DelaminatingOpen-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forcesWilliam L. Ko

Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces

William L. Ko · Ames Research Center

22 sayfa · 1990

Composite materials / Curves, Elliptic / Laminated materials / Laminates / Delaminating

Stress concentrationStress analysis of B-52 pylon hooksWilliam L. Ko

Stress analysis of B-52 pylon hooks

William L. Ko · National Aeronautics and Space Administration, Ames Researach Center, Dryden Flight Research Facility

Sayfa sayısı yok · 1985

Stress concentration

CiltApplication of finite elastic theory to the behavior of rubber-like materialsWilliam L. Ko

Application of finite elastic theory to the behavior of rubber-like materials

William L. Ko · California Institute of Technology

175 sayfa · 1963

Kategori yok

Plates (Engineering)Compressive buckling analysis of hat-stiffened panelWilliam L. Ko

Compressive buckling analysis of hat-stiffened panel

William L. Ko · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1991

Buckling (Mechanics) / Plates (Engineering)

Buckling (Mechanics)Buckling behavior of René 41 tubular panels for a hypersonic aircraft wingWilliam L. Ko

Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing

William L. Ko · National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility

Sayfa sayısı yok · 1986

Airplanes / Wings / Buckling (Mechanics)

Laminated materialsDelamination stresses in semicircular laminated composite barsWilliam L. Ko

Delamination stresses in semicircular laminated composite bars

William L. Ko · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1988

Laminated materials

ElastomersElastic constants for superplastically formed/diffusion bonded corrugated sandwich coreWilliam L Ko

Elastic constants for superplastically formed/diffusion bonded corrugated sandwich core

William L Ko · National Aeronautics and Space Administration

79 sayfa · 1980

Plastics / Elastomers

Honeycomb coresThermal behavior of a titanium honeycomb-core sandwich panelWilliam L. Ko

Thermal behavior of a titanium honeycomb-core sandwich panel

William L. Ko · National Technical Information Service, distributor]

13 sayfa · 1991

Titanium / Aerodynamic heating / Airframes / Temperature effects / Honeycomb cores

Liquid rocket propellantsThermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heatingWilliam L. Ko

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

William L. Ko · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1994

Buckling / Loads (Forces) / Cryogenic cooling / Stress analysis / Liquid rocket propellants

Buckling (Mechanics)Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing #h microformWilliam L Ko

Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing #h microform

William L Ko · For sale by the National Technical Information Service

Sayfa sayısı yok · 1986

Airplanes / Wings / Buckling (Mechanics)

Aerodynamic heating.Effect of element size on the solution accuracies of finite-element heat transfer and thermal stress analyses of space shuttle orbiterWilliam L. Ko

Effect of element size on the solution accuracies of finite-element heat transfer and thermal stress analyses of space shuttle orbiter

William L. Ko · For sale by the National Technical Information Service

Sayfa sayısı yok · 1988

Aerodynamic heating.

Structural engineeringExtension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structuresWilliam L. Ko

Extension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structures

William L. Ko · National Aeronautics and Space Administration, Dryden Flight Research Center

76 sayfa · 2011

Spherical shells / Cantilever beams / Curvature / Curved beams / Structural engineering

Flexible wingsMethods for in-flight wing shape predictions of highly flexible unmanned aerial vehiclesWilliam L. Ko

Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles

William L. Ko · National Aeronautics and Space Administration, Dryden Flight Research Center

20 sayfa · 2010

Deformation / Displacement / Shapes / Distortion / Flexible wings

Cantilever beamsImproved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strainsWilliam L. Ko

Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains

William L. Ko · National Aeronautics and Space Administration, Dryden Flight Research Center

79 sayfa · 2012

Deformation / Displacement / Transfer functions / Strain distribution / Cantilever beams

Structural strainFirst- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strainsWilliam L. Ko

First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains

William L. Ko · National Aeronautics and Space Administration, Dryden Flight Research Center

51 sayfa · 2012

Cantilever beams / Deformation / Displacement / Transfer functions / Structural strain

Fiber orientationThermal and mechanical buckling analysis of hypersonic aircraft hat-stiffened panels with varying face sheet geometry and fiber orientationWilliam L. Ko

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

William L. Ko · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1996

Mechanical properties / Aircraft structures / Finite element method / Hypersonic aircraft / Fiber orientation

Laminated materials.Mechanical and thermal buckling analysis of sandwich panels under different edge conditionsWilliam L. Ko

Mechanical and thermal buckling analysis of sandwich panels under different edge conditions

William L. Ko · National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program

Sayfa sayısı yok · 1993

Laminated materials.

Airframes -- Fatigue.Prediction of service life of aircraft structural components using the half-cycle methodWilliam L. Ko

Prediction of service life of aircraft structural components using the half-cycle method

William L. Ko · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1987

Airframes -- Fatigue.

Aspect ratio.Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methodsWilliam L. Ko

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

William L. Ko · Available from the National Technical Information Service

Sayfa sayısı yok · 1995

Aerodynamic heating. / Aerodynamic loads. / Aircraft design. / Applications programs (Computers) / Aspect ratio.

Heating.Thermostructural behavior of a hypersonic aircraft sandwich panel subjected to heating on one sideWilliam L. Ko

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

William L. Ko · National Technical Information Service, distributor]

Sayfa sayısı yok · 1997

Aerodynamic heating. / Aircraft structures. / Structural analysis. / Temperature effects. / Heating.

Thermal stresses.Thermal stress analysis of space shuttle orbiter wing skin panel and thermal protection systemWilliam L. Ko

Thermal stress analysis of space shuttle orbiter wing skin panel and thermal protection system

William L. Ko · National Aeronautics and Space Administration, Ames Researach Center, Dryden Flight Research Facility

Sayfa sayısı yok · 1987

Space shuttles. / Thermal stresses.

Metallic composites.Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environmentsWilliam L. Ko

Compressive and shear buckling analysis of metal matrix composite sandwich panels under different thermal environments

William L. Ko · National Technical Information Service, distributor]

Sayfa sayısı yok · 1993

Buckling (Mechanics) / Metallic composites.

Stress concentrationStress concentration around a small circular hole in the HiMAT composite plateWilliam L Ko

Stress concentration around a small circular hole in the HiMAT composite plate

William L Ko · National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility

Sayfa sayısı yok · 1986

Anisotropy / Stress concentration