Solution of the Compressible Navier-Stokes Equations of Motion by Chebyshev Polynomials for Laminar Shock-Boundary Layer Flow

摘要

This time dependent, compressible, 2-D Navier-Stokes equations of motion are solved by full pseudo spectral means. The flow solved for is a laminar oblique shock-boundary layer interaction. Comparison of the numerical surface pressure field with the experimental one is very good.