Abstract
When we analyze the compressible flow field including shock wave by computational calculation, the solution diverges because of the discontinuity of shock. If we use transformed-Fluid-in-Cell Method, the discontinuity is artificially smoothed and we can analyze the flow field stably. But in the analysis by transformed-Fluid-in-Cell Method, mesh form influences the solution. So we applied the Adaptive Mesh Method to transformed-Fluid-in-Cell Method and got the solution not influenced by mesh form in the analysis of super sonic flow field around blunt nosed body.
