The 3D Computational Investigation of Film Cooling Effectiveness for Turbine Nozzle Vanes with “Meridian Constriction” and Shaped Film-Cooling Holes
Crossref DOI link: https://doi.org/10.3103/S1068799818010087
Published Online: 2018-10-11
Published Print: 2018-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Gorelov, Yu. G.
Tyul’kov, K. V.
Text and Data Mining valid from 2018-01-01
Article History
Received: 13 September 2017
First Online: 11 October 2018