Transforming Energy through Computational Excellence. Exascale Computing: Combustion; Simulating Effects of Fuel Injection Location in Supersonic Jet Engines

Research output: NRELFact Sheet

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 languageAmerican English
StatePublished - 2021

NREL Publication Number

  • NREL/FS-2C00-80880

Keywords

  • adaptive mesh refinement
  • combustion
  • exascale
  • fuel injection
  • pele
  • supersonic jet

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