A Numerical Approach and Study of the Shock-Wave Structure of Supersonic Jet Flow in a Nozzle
Description
Toolbox-ID
jz000104-0126
Identifier(s)
https://tustorage.ulb.tu-darmstadt.de/handle/tustorage/18244
Publisher
MDPI AG
License
https://creativecommons.org/licenses/by/4.0/
Subject(s)
DDC(s)
530