Abstract
An efficient numerical algorithm is presented for solving the unsteady compressible Navier-Stokes equations. The solution procedure is based on a finite volume Runge-Kutta time stepping scheme developed by Jameson, Schmidt and Turkel. The algorithm is used to calculate the flow fields due to shock boundary layer interaction on a flat plate and an airfoil. Numerical results are compared with the calculations of other investigators, asymptotic theory, and experimental data. (A)
| Original language | English |
|---|---|
| Journal | [No source information available] |
| State | Published - 1985 |