Gas Turbine Combustion

Abstract

THE design of gas turbine combustion chambers and the demands made upon the various components as operating conditions become tougher have been considered at a symposium which has highlighted the compromises necessary to achieve optimum performance. The papers and discussions at this symposium fall into four categories: Alternative Fuels and Fuel Injection; Combustor Development; Soot and Radiation; and Combustion Modelling.

Citation

Ford, T., CEng and MRAeS (1990), "Gas Turbine Combustion", Aircraft Engineering and Aerospace Technology, Vol. 62 No. 5, pp. 21-22. https://doi.org/10.1108/eb036941