Accession Number:

AD0684693

Title:

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

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1968-09-27

Pagination or Media Count:

13.0

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.

Subject Categories:

  • Thermodynamics
  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE