Using a shock control bump to improve the performance of an axial compressor blade section
Crossref DOI link: https://doi.org/10.1007/s00193-016-0672-x
Published Online: 2016-07-02
Published Print: 2017-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Mazaheri, K.
Khatibirad, S.
License valid from 2016-07-02