An Investigation of Gas Turbine Combustors with High Inlet Air Temperatures. Part 2; Heat Transfer
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1971
- Accession Number
- AD0884359
Entities
People
- Arthur M. Mellor
- Clifton W. Owens
Organizations
- Purdue University