Particle Simulation of Hypersonic Flow

Abstract

A particle code for simulating a rarefied hypersonic flow is developed which accounts for a multiple species gas in thermochemical nonequilibrium and which takes advantage of the parallel architecture of the Intel iPSC/860 supercomputer. Various tests were conducted using a generic blunt body consisting of a hemispherically blunted 60-degree half-angle cone at angle of attack. The different tests conducted show that the performance of the parallel code using 512 nodes exceeds by an order of magnitude the performance obtained for a highly vectorized code run on a single processor of the Cray YMP, that scaleup is found to be nearly linear with the number of processors used, that run time can be greatly reduced by employing a large number of particles, and that runs with 67.5 million particles can be carried out when employing the large memory of the Intel iPSC/860. Other results relate to different applications of the code for studying the near-continuum state of a gas near a cold solid boundary.

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Document Details

Document Type
Technical Report
Publication Date
May 26, 1993
Accession Number
ADA267185

Entities

People

  • Donald Baganoff

Organizations

  • Stanford University

Tags

Communities of Interest

  • Energy and Power Technologies
  • Materials and Manufacturing Processes
  • Space

DTIC Thesaurus Topics

  • Algorithms
  • Blunt Bodies
  • Boundary Layer
  • Chemical Kinetics
  • Communication Systems
  • Computations
  • Computer Programming
  • Fluid Dynamics
  • Gas Flow
  • Geometric Forms
  • Geometry
  • Hypersonic Flow
  • Knudsen Number
  • Mach Number
  • Monte Carlo Method
  • Physics Laboratories
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Fluid Dynamics.
  • Parallel and Distributed Computing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow