An FV-EE model to predict lean blowout limits for gas turbine combustors with different structures and sprays

Author:

WANG Xiwei,HUANG Yong,LIU Yunfeng,WU Yufan,WANG Hongyan

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference34 articles.

1. Lean blow-out studies in a swirl stabilized annular gas turbine combustor;Mishra;Int J Turbo Jet Engines,2015

2. Experimental characterization of premixed flame in gas turbine combustor with spectroscopy and RGB analysis;Kumar,2013

3. Technology for the design of high temperature rise combustors;Bahr,1985

4. Experimental study on NOx emission correlation of fuel staged combustion in a LPP combustor at high pressure based on NO-chemiluminescence;Wang;Chin J Aeronaut,2020

5. Experimental investigations of the spray structure and interactions between sectors of a double-swirl low-emission combustor;Fan;Chin J Aeronaut,2020

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