1. The Rayleigh integral is always positive in steadily operated combustors;Bruno;Proc. Combust. Inst.,2022
2. Factors determining the flame configuration and affecting combustion stability in gas turbine combustors;Bulysova;Power Technol. Eng.,2020
3. Effects of gas nozzle and resonators on acoustic characteristics of combustion chamber;Cao;J. Aerosp. Power,2019
4. Effects of fuel variation and inlet air temperature on combustion stability in a gas turbine model combustor;Chen;Aerosp. Sci. Technol.,2019
5. Fully Compressible Numerical Simulation Study of Mechanisms and Influencing Factors of Combustion Instability;Cheng,2021