Three-Dimensional, Primitive-Variable Model for Solid-Fuel Ramjet Combustion.

Abstract

A three-dimensional computer code has been developed for the solid-fuel ramjet combustion process. The code includes finite-rate chemical kinetics and has been used to predict the combustion behavior for axial inlet, side-dump inlet and bypass configurations. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1984
Accession Number
ADA138756

Entities

People

  • D. W. Netzer
  • T. Milshtein

Organizations

  • Naval Postgraduate School

Tags

Communities of Interest

  • Materials and Manufacturing Processes
  • Weapons Technologies

DTIC Thesaurus Topics

  • Boundary Layer
  • Chambers
  • Chemical Kinetics
  • Combustion
  • Computational Fluid Dynamics
  • Computer Programs
  • Computers
  • Differential Equations
  • Equations
  • Flow
  • Flow Fields
  • Geometry
  • Heat Transfer
  • Kinetics
  • Solid Fuels
  • Three Dimensional
  • Two Dimensional

Fields of Study

  • Physics

Readers

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