Secondary flow visualization on stagnation row of a combined impingement and film cooled high-pressure gas turbine nozzle guide vane using PIV technique
Crossref DOI link: https://doi.org/10.1007/s12650-017-0434-6
Published Online: 2017-05-10
Published Print: 2017-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kukutla, Pol Reddy
Prasad, B. V. S. S. S.
License valid from 2017-05-10