Survey of Numerical Methods for the Calculation of Inviscid, Possibly Rotational Euler Flows around Aeronautical Configurations

摘要

Numerical methods for the calculation of inviscid Euler flows are reviewed. For aerodynamic applications, the existing methods are accurate and cheap enough. However, shocks and vortex sheets may have to be better modeled to achieve higher numerical accuracy. Computation times can be reduced by applying multigrid methods.