Difference in Thermo-Acoustic Instability Frequency Between Partially and Fully Premixed Flames
Author:
Affiliation:
1. Seoul National University, Seoul 08826, Republic of Korea
2. Agency for Defense Development, Daejeon 34186, Republic of Korea
3. Incheon National University, Incheon 22012, Republic of Korea
Funder
National Research Foundation of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38534
Reference30 articles.
1. LieuwenT. C.YangV., Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, and Modeling, Progress in Astronautics and Aeronautics, Vol. 210, AIAA, Reston, VA, 2005, pp. 43–63.
2. The Effect of Confinement on the Structure and Dynamic Response of Lean-Premixed, Swirl-Stabilized Flames
3. Suppression of combustion instability by geometrical design of the bluff-body stabilizer
4. Effects of hydrogen addition on flame structure and forced flame response to velocity modulation in a turbulent lean premixed combustor
5. Parameter variations and the effects of hydrogen: An experimental investigation in a lean premixed low swirl combustor
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