Accession Number:

ADA191033

Title:

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

Personal Author(s):

Corporate Author:

NAVAL RESEARCH LAB WASHINGTON DC

Report Date:

1988-03-18

Abstract:

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.

Descriptive Note:

Memorandum rept.,

Pages:

0023

Descriptors:

Identifiers:

Subject Categories:

Communities Of Interest:

Modernization Areas:

File Size:

1.08MB

View The Document