Numerical Investigation of Primary Combustion Zone of Aeroengine Combustor-Reference-Cited by-同舟云学术

Numerical Investigation of Primary Combustion Zone of Aeroengine Combustor

Published:2013-09 Issue: Volume:401-403 Page:214-217
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Wang Ping¹,Li Yong Ze¹,Sun Bo¹,Guo Hui¹,Chen Yu¹

Affiliation:

1. Aviation University of Air Force

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.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.401-403.214.pdf

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