Solution of the Compressible Navier-Stokes Equations of Motion by Chebyshev Polynomials for Laminar Shock-Boundary Layer Flow.
NAVAL RESEARCH LAB WASHINGTON DC
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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. Keywords Computations, Shock waves.
- Fluid Mechanics