Abstract
Computational tractable simulations using an adaptive-mesh-refinement solverfor compressible reacting flows help researchers understand how variations in fuel injection location within the supersonic flow cavity impacts combustion efficiency. By identifying the important physical determinants of the combustion processes, this study shows a promising pathway to improving flame stability and combustion efficiency, as well as reducing emissions.
| Original language | American English |
|---|---|
| Publisher | National Laboratory of the Rockies (NLR) |
| State | Published - 2021 |
NLR Publication Number
- NREL/FS-2C00-80880
Keywords
- adaptive mesh refinement
- combustion
- exascale
- fuel injection
- pele
- supersonic jet
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