NASA NTRS · 19840000129
Computation of Three-Dimensional Combustor Performance
Abstract
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.
Keep this discovery
Explore connections, maps & timelines
Srivatsa, S.. 1985-01-01. Computation of Three-Dimensional Combustor Performance. https://ntrs.nasa.gov/citations/19840000129
Cite the original work for its findings. Save a collection to share your selection of sources.