Aircraft Engine Combustion Chamber Performances-Numerical Evaluation

Ionică Cîrciu; Constantin Rotaru; Doru Luculescu; Cristian Constantinescu

doi:10.4028/www.scientific.net/AMM.811.167

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 811Aircraft Engine Combustion Chamber...

Aircraft Engine Combustion Chamber Performances-Numerical Evaluation

Abstract:

In this paper are presented some CFD results regarding combustion in an aircraft turbojet engine, for aviation fuels consisting of hydrocarbon mixtures. Recent achievements in chemical kinetic modeling of kerosene combustion are presented. Performance parameters investigated were combustion efficiency, unburned hydrocarbons as well as liner temperatures and smoke. The analysis is based on the theoretically and experimentally characteristics of a typical axial flow engine.

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Periodical:

Applied Mechanics and Materials (Volume 811)

Pages:

167-171

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.811.167

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Online since:

November 2015

Authors:

Ionică Cîrciu, Constantin Rotaru*, Doru Luculescu, Cristian Constantinescu

Keywords:

Aircraft Propulsion, Combustion Chamber, Turbojet

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* - Corresponding Author

References

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