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
Description
Toolbox-ID
jz000100-0013
Identifier(s)
https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/10038
Publisher
MDPI AG
License
https://creativecommons.org/licenses/by-nc-nd/4.0/
Subject(s)
DDC(s)
620