ON THE CALCULATION OF THE SIMPLEST RAMJET-TYPE COMBUSTOR

Abstract

A calculation method for the simplest ramjet-type combustor is presented. The method consists in closing the system of the basic gas-dynamic equations (of fuel-mixture flow) within a cylindrical tube with a point-ignition source, by introducing an auxiliary condition which defines the dependence of the width of the combustion zone on the distance to the ignition source. The results of the calculation were compared with some experimental data and were found to be in good agreement with them.

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Document Details

Document Type
Technical Report
Publication Date
Sep 20, 1962
Accession Number
AD0621693

Entities

People

  • K. P. Vlasov

Organizations

  • Library of Congress

Tags

Communities of Interest

  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Boundaries
  • Climate Change
  • Combustion
  • Combustion Products
  • Combustors
  • Equations
  • Experimental Data
  • Flame Propagation
  • Flames
  • Flow
  • Heat Energy
  • Ignition
  • Ionization
  • Measurement
  • Photography
  • Static Pressure
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Internal Combustion Engine (ICE) Technology.
  • Spectroscopy.