Experimental study on flame/flow dynamics in a multi-nozzle gas turbine model combustor under thermo-acoustically unstable condition with different swirler configurations-Reference-Cited by-同舟云学术

Experimental study on flame/flow dynamics in a multi-nozzle gas turbine model combustor under thermo-acoustically unstable condition with different swirler configurations

Published:2020-03 Issue: Volume:98 Page:105692
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Ruan Can,Chen Feier,Yu Tao,Cai Weiwei,Li Xinling,Lu Xingcai

Funder

National Natural Science Foundation of China

Program of Shanghai Subject Chief Scientist

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

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3. Dynamics and stability of lean-premixed swirl-stabilized combustion;Huang;Prog. Energy Combust. Sci.,2009

4. A review of active control approaches in stabilizing combustion systems in aerospace industry;Zhao;Prog. Aerosp. Sci.,2018

5. Prediction of stability behaviors of longitudinal and circumferential eigenmodes in a choked thermoacoustic combustor;Li;Aerosp. Sci. Technol.,2015

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