Investigation into the cause of high multi-mode combustion instability of H2/CO/CH4 syngas in a partially premixed gas turbine model combustor-Reference-Cited by-同舟云学术

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Investigation into the cause of high multi-mode combustion instability of H2/CO/CH4 syngas in a partially premixed gas turbine model combustor

Published:2015 Issue:3 Volume:35 Page:3263-3271
ISSN:1540-7489
Container-title:Proceedings of the Combustion Institute
language:en
Short-container-title:Proceedings of the Combustion Institute

Author:

Lee Min Chul,Yoon Jisu,Joo Seongpil,Kim Jeongjin,Hwang Jeongjae,Yoon Youngbin

Funder

the Mid-career Researcher Program of NRF MEST

New/Renewable Energy Technology Development Program

Publisher

Elsevier BV

Subject

Physical and Theoretical Chemistry,Mechanical Engineering,General Chemical Engineering

Reference20 articles.

1. A Mechanism of Combustion Instability in Lean Premixed Gas Turbine Combustors

2. Combustion dynamics of turbulent swirling flames

3. Influence of the Combustor Aerodynamics on Combustion Instabilities From Equivalence Ratio Fluctuations

4. A review of oscillation mechanisms and the role of the precessing vortex core (PVC) in swirl combustion systems

5. Interference mechanisms of acoustic/convective disturbances in a swirl-stabilized lean-premixed combustor

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4. Numerical Simulation of H2 Addition Effect to CH4 Premixed Turbulent Flames for Gas Turbine Burner;Journal of Applied Fluid Mechanics;2024-08-01

5. Combustion instability characteristics via fuel nozzle modification in a hydrogen and natural gas Co-firing gas turbine combustor;International Journal of Hydrogen Energy;2024-08

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