Transition modelling implications in the CFD analysis of a turbine nozzle vane cascade tested over a range of Mach and Reynolds numbers
Crossref DOI link: https://doi.org/10.1007/s11630-015-0818-7
Published Online: 2015-11-10
Published Print: 2015-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Marconcini, Michele
Pacciani, Roberto
Arnone, Andrea
Text and Data Mining valid from 2015-11-01
