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
01.01.1985
Sonstige
Keine Angabe
Englisch
Three dimensional hot flow computation of the aero gas turbine combustor
British Library Conference Proceedings | 2000
|Three-dimensional NOx modeling for rich/lean combustor
AIAA | 1993
|