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Title: Correlations of soot formation in turbojet engines and in laboratory flames

Conference · · Am. Soc. Mech. Eng., (Pap.); (United States)
OSTI ID:5107854

Smoke related performance of both jet engine and research combustors has been correlated with several fuel properties. The smoke related data included: smoke number, liner temperature rise, and radiation flux to the combustor wall; fuel parameters included: percent hydrogen, percent aromatic, percent polycyclic aromatic, smoke point, and the threshold soot index, TSI. The research combustor results correlated best with the threshold sooting index. While some correlations with engine performance were excellent, no single fuel property was generally useful in evaluating smoke related performance, mainly because of insufficient data on the fuels tested in the jet engine programs. It is, however, demonstrated that fuel composition plays a dominant role in determining smoke related engine parameters.

Research Organization:
AeroChem Research Laboratories, Inc., Princeton, New Jersey
OSTI ID:
5107854
Report Number(s):
CONF-840611-
Journal Information:
Am. Soc. Mech. Eng., (Pap.); (United States), Vol. 84-GT-108; Conference: International gas turbine conference and exhibit, Amsterdam, Netherlands, 4 Jun 1984
Country of Publication:
United States
Language:
English