Impact of Leakage Inlet Swirl Angle in a Rotor–Stator Cavity on Flow Pattern, Radial Pressure Distribution and Frictional Torque in a Wide Circumferential Reynolds Number Range
Description
Toolbox-ID
jz000095-0015
Identifier(s)
https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/9246
Publisher
MDPI AG
License
https://creativecommons.org/licenses/by/4.0/
Subject(s)
DDC(s)
620