Effects of airfoil-probe tubes on the flow field of a compressor cascade
Crossref DOI link: https://doi.org/10.1007/s11630-017-0945-4
Published Online: 2017-07-19
Published Print: 2017-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Ma, Hongwei
Jin, Chao
Zhao, Lianpeng
Ma, Rong
License valid from 2017-07-19
