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T. Nonweiler

  • A method for the numerical evaluation of an integralA method for the numerical evaluation of an integral
  • A new series of low drag aerofoilsA new series of low drag aerofoils
  • A resume of maximum lift data for symmetrical wings, with various high-lift aidsA resume of maximum lift data for symmetrical wings, with various high-lift aids
  • Skin temperatures and heat transfer over wedge wings at extreme speedsSkin temperatures and heat transfer over wedge wings at extreme speeds
  • Surface conduction of the heat transferred from a boundary layerSurface conduction of the heat transferred from a boundary layer
  • The air resistance of racing cyclistsThe air resistance of racing cyclists
  • The laminar boundary layer in slip flowThe laminar boundary layer in slip flow
  • The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary sectionThe theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section
  • The two-dimensional laminar boundary layer at hypersonic speedsThe two-dimensional laminar boundary layer at hypersonic speeds
  • The wave drag of highly-swept wingsThe wave drag of highly-swept wings
  • Theoretical stability derivatives of a highly swept delta wing and slender body combinationTheoretical stability derivatives of a highly swept delta wing and slender body combination