The Influence of Combustor Swirl on Pressure Losses and the Propagation of Coolant Flows at the Large Scale Turbine Rig (LSTR): Experimental and Numerical Investigation

Holger WerschnikMarius SchneiderJanina HerrmannDimitri IvanovHeinz-Peter SchifferChristoph Lyko2024-08-262024-08-262017jz000100-0013https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/10038620The Influence of Combustor Swirl on Pressure Losses and the Propagation of Coolant Flows at the Large Scale Turbine Rig (LSTR): Experimental and Numerical InvestigationArticlehttps://doi.org/10.3390/ijtpp2030012