Abstract: In this paper, we experimentally investigate the thermoacoustic instability issue in an annular combustor with 16 oblique-injecting premixed swirling burners. It is demonstrated that there exist three dominant modes in a ...

Abstract: This study focuses on the enginerepresentative MT1 transonic highpressure turbine. Simulated by use of wallmodeled largeeddy simulations (LES) with three different subgrid scale (SGS) closures, mean pressure profiles across ...

Abstract: Indirect combustion noise, generated by the acceleration and distortion of entropy waves through the turbine stages, has been shown to be the dominant noise source of gas turbines at lowfrequencies and to impact the ...

Abstract: Experiments on kerosene spray through a single-hole nozzle are carried out under various ambient pressures ranging from 1.4 to 5.6 MPa. High-speed schlieren photography is used to capture the time-dependent images of the ...