Immersed Boundary Method for Numerical Simulation of Supersonic Flow over Blunt Bodies on Rectangular Grids
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
AbstractArticle is dedicated to generalization of ghost-cell immersed boundary method for solving problems of computational aerohydrodynamics in complex geometrical domains, using rectangular grids. High efficiency of this method is demonstrated on a benchmark problem of supersonic flow over the circular cylinder. Comparative analysis has shown good agreement of obtained results with benchmark solutions.