Existing steady-state 3-D computer program for calculating gasturbine flow fields modified to include computation of soot and nitrogen oxide emission. In addition, radiation calculation corrected for soot particles. These advanced tools offer potential of reducing design and development time required for gas-turbine combustors.
Computation of Three-Dimensional Combustor Performance
NASA Tech Briefs ; 8 , 3
1985-01-01
Miscellaneous
No indication
English
Three dimensional hot flow computation of the aero gas turbine combustor
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