Patent · US Active

Computationally efficient reduced kinetics methodologies for jet fuels

US11914930B1 · kind B1 · utility

0Cited by
3References
14Claims
0Family size

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Key dates

Filing dateSep 11, 2013
Grant dateFeb 27, 2024
Priority date
Expiry dateAug 13, 2037

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG06F17/10
  • WIPO fieldComputer technology
  • WIPO sectorElectrical engineering

Abstract

A method for implementing a modeling tool that generates optimized reduced kinetics models for given operating conditions and a numerical scheme to speed-up kinetics evaluation of turbulent-chemistry coupling during CFD simulations. The tool is capable of predicting ignition and flameholding phenomenon for most propulsion systems, including gas turbine applications. A lumped-parameterization based optimization scheme may generate multi-step quasi-global kinetics models using laminar flame speed as the target data. This scheme may be further extended to include optimization of emission predictions such as CO and NOx.

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