A complete boundary integral formulation for compressible Navier-Stokes equations

摘要

A complete boundary integral formulation for compressible Navier-Stokes equations with time discretization by operator splitting is developed using the fundamental solutions of the Helmholtz operator equation with different order. The numerical results for wall pressure and wall skin friction of two-dimensional compressible laminar viscous flow around airfoils are in good agreement with field numerical methods. Copyright (c) 2004 John Wiley A Sons, Ltd.