Hybrid method based on flame volume concept for lean blowout limits prediction of aero engine combustors
Authors:
- Lei SunLSLei Sun
- Yong HuangYHYong Huang
- Xiwei WangXWXiwei Wang
- Zekun ZhengZZZekun Zheng
- Ruixiang WangRWRuixiang Wang
- Xiang FengXFXiang Feng
Open Access
- 1 May 2021
- journal article
- research article
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 34 (5) , 425-437
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China
- National Science and Technology Major Project
This publication has 28 references indexed in Scilit:
- FIA method for LBO limit predictions of aero-engine combustors based on FV modelAerospace Science and Technology, 2013
- Experimental Study on Emission Performance of an LPP/TVCChinese Journal of Aeronautics, 2012
- Aircraft engines’ needs from combustion science and engineeringCombustion and Flame, 2012
- Combustion and emission modelling near lean blow-out in a gas turbine engineProgress in Computational Fluid Dynamics, An International Journal, 2005
- Lean blowout model for a spray-fired swirl-stabilized combustorProceedings of the Combustion Institute, 2000
- Three-dimensional combustor performance validation with high-densityfuelsJournal of Propulsion and Power, 1990
- Correlation of Lean Blowoff of Gas Turbine Combustors Using Alternative FuelsJournal of Energy, 1983
- Weak Extinction Limits of Turbulent Flowing MixturesJournal of Engineering for Power, 1979
- Characteristic time correlation for lean blowoff of bluff-body-stabilized flames☆Combustion and Flame, 1979
- Flame Stabilization in Simplified Prevaporizing, Partially Vaporizing, and Conventional Gas Turbine CombustorsJournal of Energy, 1978