Thermoacoustic Instability Characteristics and Flame/Flow Dynamics in a Multinozzle Lean Premixed Gas Turbine Model Combustor Operated with High Carbon Number Hydrocarbon Fuels-Reference-Cited by-同舟云学术

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Thermoacoustic Instability Characteristics and Flame/Flow Dynamics in a Multinozzle Lean Premixed Gas Turbine Model Combustor Operated with High Carbon Number Hydrocarbon Fuels

Published:2021-01-05 Issue:2 Volume:35 Page:1701-1714
ISSN:0887-0624
Container-title:Energy & Fuels
language:en
Short-container-title:Energy Fuels

Author:

Ruan Can¹,Zhang Linqi¹,Chen Feier¹,Yu Tao¹,Cai Weiwei¹,He Zhuoyao¹,Qian Yong¹,Lu Xingcai¹^ORCID

Affiliation:

1. School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, P. R. China

Funder

Program of Shanghai Subject Chief Scientist

National Natural Science Foundation of China

Publisher

American Chemical Society (ACS)

Subject

Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Link

https://pubs.acs.org/doi/pdf/10.1021/acs.energyfuels.0c03165

Reference62 articles.

1. Review on Premixed Combustion Technology: Stability, Emission Control, Applications, and Numerical Case Study

2. Principles of non-intrusive diagnostic techniques and their applications for fundamental studies of combustion instabilities in gas turbine combustors: A brief review

3. Numerical prediction of swirl burner geometry effects on NOx emission and combustion instability in heavy oil-fired boiler

4. Impact of symmetry breaking on the Flame Transfer Function of a laminar premixed flame

5. Effects of annular N2/O2 and CO2/O2 jets on combustion instabilities and NOx emissions in lean-premixed methane flames

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