617 Numerical Simulation of Supersonic Flows using a Solution-adaptive Unstructured Grid Solver
Details
Our solution-adaptive scheme for the unstructured grid using the edge algorithm was applied to the reflection problem of oblique shock waves with conditions of Mach number 2.0 and deviation angle about 11 degrees. The result shows that our adaptation scheme captures the regular reflection on both the upper and the lower walls and the expansion fan more clearly. Therefor the applicability of our scheme was confirmed.
