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

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.

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Document Details

Document Type
Technical Report
Publication Date
Mar 18, 1988
Accession Number
ADA191033

Entities

People

  • Leonidas Sakell

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Boundary Layer Flow
  • Chebyshev Polynomials
  • Computational Fluid Dynamics
  • Computational Science
  • Differential Equations
  • Equations
  • Equations Of Motion
  • Euler Equations
  • Fluid Dynamics
  • Layers
  • Navier Stokes Equations
  • Partial Differential Equations
  • Pressure Distribution
  • Turbulent Mixing
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Linear Algebra