ENGINEERING METHOD FOR THERMODYNAMIC CALCULATIONS OF JET-TYPE COMBUSTION CHAMBERS USING HYDROCARBON FUEL AND AIR,

Abstract

A method is presented for determining the temperature and composition of the working substance in a combustion chamber and at the nozzle exit. The method is suitable for any fuel with a C, H, O, and N composition. The working substance coefficient and temperature in the combustion chamber and at the nozzle exit cross-section are found from a set of equations representing the combustion process at constant pressure and isoentropic expansion up to a given pressure at the nozzle exit cross-section.

Document Details

Document Type
Technical Report
Publication Date
Sep 27, 1968
Accession Number
AD0684693

Entities

People

  • I. P. Goldaev
  • V. P. Cherepanov

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Chambers
  • Chemical Reactions
  • Coefficients
  • Combustion
  • Combustion Chambers
  • Engineering
  • Engines
  • Equations
  • Exothermic Reactions
  • Heat Engines
  • Heat Transfer Devices
  • Hydrocarbon Fuels
  • Hydrocarbons
  • Ignition
  • Internal Combustion Engines

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.