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  1. Performance improvement of supersonic nozzles design using a high-temperature model
  2. Rapid design method and new contours for a class of three dimensional supersonic nozzle of arbitrary exit cross section
  3. High temperature gas effect on the Prandtl-Meyer function with application for supersonic nozzle design
  4. Numerical computation of shear stress in a complex cross section subjected to a shear force and application to airfoils