Accession Number : AD0775060

Title :   Development of a Combustor Flow Analysis: Part II. Experimental Studies.

Descriptive Note : Final rept. 1 Jun-30 Sep 73,

Corporate Author : UNITED AIRCRAFT RESEARCH LABS EAST HARTFORD CONN

Personal Author(s) : Anasoulis,Robert F. ; McDonald,Henry

Report Date : 28 FEB 1974

Pagination or Media Count : 38

Abstract : Measurements were conducted in a full annular premixed combustor to provide profiles of UHC, CO, CO2, O2, N2, H2, NO, NOx and temperature at various axial locations. The work was performed to further develop an existing computational procedure for predicting the performance and exhaust emission characteristics of can-annular or annular gas turbine combustors. The results, however, were also found to be useful in showing areas within the combustor where emissions, particularly NOx, are formed. (Modified author abstract)

Descriptors :   *Combustion chambers, *Gas turbines, *Exhaust gases, Temperature, Gas analysis, Profiles, Position(Location)

Subject Categories : Combustion and Ignition
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE