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William L. Ko

  • Application of finite elastic theory to the behavior of rubber-like materialsApplication of finite elastic theory to the behavior of rubber-like materials
  • Buckling behavior of René 41 tubular panels for a hypersonic aircraft wingBuckling behavior of René 41 tubular panels for a hypersonic aircraft wing
  • Combined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environmentsCombined-load buckling behavior of metal-matrix composite sandwich panels under different thermal environments
  • Delamination stresses in semicircular laminated composite barsDelamination stresses in semicircular laminated composite bars
  • Elastic constants for superplastically formed/diffusion bonded corrugated sandwich coreElastic constants for superplastically formed/diffusion bonded corrugated sandwich core
  • Extension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structuresExtension of Ko straight-beam displacement theory to deformed shape predictions of slender curved structures
  • Finite-element reentry heat-transfer analysis of space shuttle orbiterFinite-element reentry heat-transfer analysis of space shuttle orbiter
  • First- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strainsFirst- and second-order displacement transfer functions for structural shape calculations using analytically predicted surface strains
  • Improved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strainsImproved displacement transfer functions for structure deformed shape predictions using discretely distributed surface strains
  • Mechanical- and thermal-buckling behavior of rectangular plates with different central cutoutsMechanical- and thermal-buckling behavior of rectangular plates with different central cutouts
  • Methods for in-flight wing shape predictions of highly flexible unmanned aerial vehiclesMethods for in-flight wing shape predictions of highly flexible unmanned aerial vehicles
  • Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite facesOpen-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces