Accession Number:

AD0884359

Title:

An Investigation of Gas Turbine Combustors with High Inlet Air Temperatures. Part 2; Heat Transfer

Descriptive Note:

Annual rept. no. 2, Mar 1970-Mar 1971

Corporate Author:

PURDUE UNIV LAFAYETTE IN JET PROPULSION CENTER

Personal Author(s):

Report Date:

1971-03-01

Pagination or Media Count:

111.0

Abstract:

The wall temperature distribution of a combustion chamber is a function of the various heat transfer processes existing in the chamber and annulus. The basic turbulent conservation equations of mass, momentum, species, and energy are developed in an effort to provide an analytical rather than empirical method of determining the temperature distribution. However, the inclusion of radiation energy exchange using the radiative transport theory and the fact that the chamber flow is not one dimensional makes a closed form solution to the problem mathematically impossible.

Subject Categories:

  • Combat Vehicles
  • Thermodynamics
  • Combustion and Ignition
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE