The nonlinear bifurcation behavior of two self-excited interacting swirl flames was
investigated in a model lean-premixed gas turbine combustor. We examined the system's …

Dynamic mode decomposition (DMD) technique is applied to analyze combustion
instabilities in a model gas turbine combustor. The flame transfer function (FTF) obtained by …

Transverse acoustic mode in annular combustion chambers affects air-fuel mixing
characteristics in the nozzle and can result in heat release fluctuations in the combustor. In …

Entropy waves (or hot spots) in a gas turbine combustor are generated by irregular heat
release from flames, then can be coupled with acoustic waves when they are accelerated at …

The nonlinear bifurcation behavior of two self-excited interacting swirl flames was
investigated in a model lean-premixed gas turbine combustor. We examined the system's …

Experiments were carried out to study the flame liftoff height (FLH) and flame stabilization at
the fuel-lean region in CH₄/Air premixed flames of a low-swirl combustor. The burner used …

The post-processing analysis tools, Short Time Fourier Transform (STFT) and Dynamic
Mode Decomposition (DMD) were applied to analyze dynamic characteristics of the …

Combustion instability of synthetic gas in a partially-premixed combustor has been
numerically investigated by varying H₂ percentage of the fuel composition. During …

Entropy waves (or hot spots) in a gas turbine combustor are generated by irregular heat
release from flames, then can be coupled with acoustic waves when they are accelerated at …

Transverse acoustic mode in annular combustion chambers affects air-fuel mixing
characteristics in the nozzle and can result in heat release fluctuations in the combustor. In …