Abstract: Large eddy simulations (LES) are performed of a bluffbody–stabilized flame with discrete liquid fuel injectors located just upstream of the bluffbody trailing edge in a socalled “closecoupledâ€‌ configuration. Nonreacting ...

Abstract: Accurate numerical prediction of surface heat transfer in the presence of film cooling within aero-engine sub-components, such as blade effusion holes and combustor liners, has long been a goal of the aero-engine industry. ...

Abstract: In this paper, we present combustor acoustics in a high-pressure liquid-fueled rich burn—quick quench—lean burn (RQL) styled swirl combustor with two separate fuel circuits. The fuel circuits are the primary (which has a ...