Investigation of the compressible flow through the tip-section turbine blade cascade with supersonic inlet
Crossref DOI link: https://doi.org/10.1007/s11630-016-0844-0
Published Online: 2016-07-02
Published Print: 2016-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Luxa, Martin
Příhoda, Jaromír
Šimurda, David
Straka, Petr
Synáč, Jaroslav
License valid from 2016-04-01