Temperature rise v. fuel/air ratio
Subtitle: for combustion of a gas turbine fuel of nominal composition H 13.92% C 86.08% by mass, having a net calorific value Qnet,p=43 100 kJ/kg
By: prepared by G.F.C. Rogers and Y.R. Mayhew.
Contributors: Mayhew, Y. R. 1924-
Publisher: Blackwell
Published: 1979
Place of publication: [Oxford]
Language: eng