IGTC-42 NO_x Predictions for Aerocombustors and Gas Turbine Engines Based on Flamelet Model for Turbulent Diffusion Combustion(Session B-5 NUMERICAL ANALYSIS OF COMBUSTION)

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概要

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• An integral method for NO_x emission predictions was developed on the base of the flamelet model consideration of the chemical processes in reaction zones taking into account both detailed combustion chemistry and chemistry/small-scale turbulence interaction. The capability of the method to predict NO_x emissions with the accuracy within 10-20% is demonstrated for almost 50 real combustors of different aircraft engines: turbofans, turbojets, turboprops, turboshafts and auxiliary power units, operated on kerosene, natural gas (methane) and hydrogen.

• 社団法人日本ガスタービン学会の論文

著者

• Volkov D.v.

  Central Institute Of Aviation Motors (ciam)

• Buriko Y.Y.

  Central Institute of Aviation Motors (CIAM)

• Gorbatko A.A.

  Central Institute of Aviation Motors (CIAM)

• Tchepin S.A.

  Central Institute of Aviation Motors (CIAM)

• Zaitsev S.A.

  Central Institute of Aviation Motors (CIAM)

関連論文

• IGTC-42 NO_x Predictions for Aerocombustors and Gas Turbine Engines Based on Flamelet Model for Turbulent Diffusion Combustion(Session B-5 NUMERICAL ANALYSIS OF COMBUSTION)

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