Full Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed
Description
Toolbox-ID
jz000093-0005
Identifier(s)
https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/9944
Publisher
MDPI AG
License
https://creativecommons.org/licenses/by-nc-nd/4.0/
Subject(s)
DDC(s)
620