Abstract: In the present work, the turbulent flow fields in a static and rotating ribbed channel representative of an aeronautical gas turbine are investigated by the means of wall-resolved compressible large-Eddy simulation (LES). ...

Abstract: Nowadays, the lack of confidence in the prediction of combustorturbine interactions and more specifically our ability to predict the migration of hot spots through this interface leads to the application of extra safety ...

Abstract: To deepen the knowledge of the interaction between modern lean burn combustors and high pressure (HP) turbines, a nonreactive real scale annular trisector combustor simulator (CS) has been assembled at University of Florence ...