Numerical Modelling of Ramjet Combustors.

Abstract

The present work deals with development of computer codes for modelling of gas turbine combustors to ramjet combustor configurations. In particular, the STARPIC code of Lilley and Rhode has been expanded to include reacting compressible flows. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1983
Accession Number
ADA129631

Entities

People

  • Warren H. Harch

Organizations

  • Wright Laboratory

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Chemical Kinetics
  • Chemical Reactions
  • Combustion
  • Computational Fluid Dynamics
  • Difference Equations
  • Differential Equations
  • Flow
  • Flow Visualization
  • Gas Turbines
  • Gaseous Fuels
  • Kinetic Energy
  • Materials Science
  • Measurement
  • Ramjet Engines
  • Three Dimensional
  • Turbines
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Computational Fluid Dynamics (CFD)
  • Internal Combustion Engine (ICE) Technology.