Abstract: The effects of the shock wave and the expansion fan on the flat plate film cooling are numerically studied under the supersonic condition with inclined cylindrical film holes. A triangular-shaped shock generator is applied, ...

Abstract: A new design method of scramjet nozzles within predetermined geometrical space is proposed to optimize the nozzle aerodynamic performance. The main characteristic of the proposed method is that the design factors and flow ...

Abstract: A design method on scramjet nozzles is proposed to satisfy the requirements of nozzle positions and geometrical constraints. The proposed method adopts the inverse design concept and maximum thrust theory to achieve a good ...