Pseudospectral Solution of Inviscid Flows with Multiple Discontinuities.

Abstract

The author has shown that a pseudospectral technique may be coupled with fourth-order artificial viscosity and spectral filtering to solve inviscid flow fields in which a single discontinuity is present. The flow fields treated in this manner have been both one and two dimensional in character; the former consisting of a shock wave propagating in the coordinate direction and the latter a supersonic wedge flow. This report presents results using that same combination of smoothing techniques applied to flows where multiple discontinuities arise. The full inviscid equations of motion (Euler equations), cast in conservation law form, are used together with an Adams-Bashforth time differencing algorithm. Two classes of time dependent multiple discontinuity inviscid flows are solved: (1) a bursting diaphragm problem, in which a shock wave and contact surface discontinuity are simultaneously present, but neither have yet reached a boundary, and (2) the flowfield which arises when two normal shock waves of unequal strengths, traveling towards each other, collide and give rise to two shock waves of new and different strengths along with a contact surface discontinuity.

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Document Details

Document Type
Technical Report
Publication Date
Aug 17, 1983
Accession Number
ADA132084

Entities

People

  • L. Sakell

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Algorithms
  • Computational Fluid Dynamics
  • Computational Science
  • Computations
  • Differential Equations
  • Discontinuities
  • Equations
  • Equations Of Motion
  • Euler Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Inviscid Flow
  • Military Research
  • Shock Waves
  • Two Dimensional
  • Viscosity

Fields of Study

  • Physics

Readers

  • Atmospheric Science / Meteorology, specifically Wind Wave Turbulence.
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)

Technology Areas

  • Hypersonics