Combustion Problems of the Gas Turbine

Abstract

THIS paper will be confined to oil fuel, which has been used so far to a predominating extent in the gas turbine. It is possible that some of the general matters touched upon will be applicable to gaseous or solid fuels, such as aero‐dynamic patterns within a combustion zone, wall cooling and effects of ash.

Citation

(1951), "Combustion Problems of the Gas Turbine", Aircraft Engineering and Aerospace Technology, Vol. 23 No. 7, pp. 196-213. https://doi.org/10.1108/eb032056