On the Stability of Higher-Order Continuum (HOC) Equations for Hybrid HOC/DSMC Solvers

Abstract

Our interest in the stability analysis of the high-order continuum (HOC) equations is motivated by the relevance to the development of a hybrid method combining such equations with the Direct Simulation Monte-Carlo (DSMC) technique for the computation of hypersonic flows in all regimes continuum, transition, and rarefied. The hybrid approach allows the effects of thermophysics (thermal and chemical non-equilibrium) and turbulence to be included much more easily than in other approaches, and can easily be developed into a robust and efficient engineering tool for practical 3D hypersonic computations. Stability characteristics of model HOC equations when subjected to small disturbances are investigated. We explore the feasibility of simplified, yet accurate and numerically stable, versions of the HOC equations and extend our previous work to include multidimensional Burnett equations, with the specific example of the Augmented Burnett models. The latter is shown to have a much wider stability regime than Lumpkin's model.

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Document Details

Document Type
Technical Report
Publication Date
Jul 13, 2005
Accession Number
ADA445985

Entities

People

  • Foluso Ladeinde
  • Ramesh Agarwal
  • Xiaodan Cai

Organizations

  • Stony Brook University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Air Force Research Laboratories
  • Boltzmann Equation
  • Boundaries
  • Chemical Reactions
  • Collisions
  • Dispersion Relations
  • Engineering
  • Equations
  • Flow
  • Fluid Dynamics
  • Gas Flow
  • Hypersonic Flow
  • Knudsen Number
  • Mechanical Engineering
  • Navier Stokes Equations

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Finite Element Method (FEM) for solving Partial Differential Equations (PDEs)
  • Thermal Physics or Thermal Science.

Technology Areas

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