Particle Simulation of Hypersonic Flow

Abstract

A limitation of the DSMC method is that it does not allow efficient use of vector architectures that are predominate in current supercomputers. A new selection rule for collisions between simulated molecules is developed which is highly compatible with vectorization. The collision-selection rule is shown to give identical results to the DSMC method in predicting shock-wave structure and in predicting the correct mean-free path variation with density and temperature for power-law interactions ranging from hard sphere to Maxwell molecule. Algorithmic improvements beyond those related to vectorization issues alone are also introduced, making possible simulations of single-species, rarefied, 3D hypersonic flows employing 10 million particles and 0.5 million cells. The performance of the algorithm on the Cray-2 ranges from 1 to 2 microseconds/particle/time-step. Roughly 500 to 1000 time-steps are needed to time average the results of a simulation, leading to run times of 2 to 5 hours on the Cray-2 for large problems. Keywords: Particle method; Rarefied flow; Direct simulation; Monte Carlo; Collision selection.

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Document Details

Document Type
Technical Report
Publication Date
Apr 24, 1990
Accession Number
ADA222704

Entities

People

  • Donald Baganoff

Organizations

  • Stanford University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Algorithms
  • Boundary Layer
  • C Programming Language
  • Chemical Kinetics
  • Chemical Reactions
  • Computer Programming
  • Computers
  • Energy
  • Energy Transfer
  • Geometry
  • Heat Transfer
  • Hypersonic Flow
  • Kinetic Theory
  • Mechanics
  • Monte Carlo Method
  • Statistical Sampling
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Fluid Dynamics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight