B

7-2. Inverse design from given shock wave

Application of a transonic design concept to supersonic flow design with given shock wave

Marching procedures based on the 3D Euler equations

 

Initial conditions for transonic or supersonic inverse design

Solving an ill-posed boundary value problem

 

Basic relations for an axisymmetric method of characteristics

Creating 3D flow fields with shocks based on plane, conical or axisymmetric flows with curved shock surfaces

 

2015