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.
Gas Turbine Combustion
Aircraft Engineering and Aerospace Technology ; 62 , 5 ; 21-22
01.05.1990
2 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Engineering Index Backfile | 1942
TIBKAT | 1983
|TIBKAT | 1998
|TIBKAT | 1994
|Continuous-combustion gas turbine
Engineering Index Backfile | 1943
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