Numerical investigation of nozzle geometry influence on the vortex cooling in an actual gas turbine blade leading edge cooling system
Crossref DOI link: https://doi.org/10.1007/s00231-021-03131-9
Published Online: 2021-09-16
Published Print: 2022-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Fan, Xiaojun http://orcid.org/0000-0003-1775-5736
Xue, Yuan
Text and Data Mining valid from 2021-09-16
Version of Record valid from 2021-09-16
Article History
Received: 28 April 2021
Accepted: 9 September 2021
First Online: 16 September 2021