Numerical Investigation of Primary Combustion Zone of Aeroengine Combustor

Ping Wang; Yong Ze Li; Bo Sun; Hui Guo; Yu Chen

doi:10.4028/www.scientific.net/AMM.401-403.214

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 401-403Numerical Investigation of Primary Combustion Zone...

Numerical Investigation of Primary Combustion Zone of Aeroengine Combustor

Abstract:

Method of CFD is used in this paper to simulate and calculate velocity field, temperature field and droplet track in PCZ(primary combustion zone) under the 3D two phase turbulent combustion for the ground idling, the peak, the middling and the altitude-small lever flying conditions. By analyzing the calculation results and comparing with tests, characters of PCZ are well investigated.

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Periodical:

Applied Mechanics and Materials (Volumes 401-403)

Pages:

214-217

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.401-403.214

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Online since:

September 2013

Authors:

Ping Wang, Yong Ze Li, Bo Sun, Hui Guo, Yu Chen

Keywords:

Combustor, Numerical Simulation, Primary Combustion Zone

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