Molecular Dynamics Simulations of Supercritical Jet Mixing

Abstract

High pressure heterogeneous combustion systems typically operate trans- or supercritical: Liquid rocket engines; Gas turbine combustors; and/or Diesel engines. Quantitative assessments or validated theories characterizing propellant injection at near and supercritical conditions are currently limited.

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Document Details

Document Type
Technical Report
Publication Date
Jun 25, 2004
Accession Number
ADA446421

Entities

People

  • Karl Ludwig
  • M. M. Micci
  • R. D. Branam

Organizations

  • Pennsylvania State University

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Combustion
  • Combustion Chambers
  • Conversion
  • Diesel Engines
  • Dynamics
  • Energy
  • Energy Conversion
  • Engines
  • Equations
  • Equations Of Motion
  • Flow
  • Gas Turbines
  • High Pressure
  • Liquid Propellants
  • Measurement
  • Molecular Dynamics
  • Simulations

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Distributed Systems and Data Platform Development
  • Molecular Genetics