Transition Effect on Shock Wave Boundary Layer Interaction on Compressor Blade
Crossref DOI link: https://doi.org/10.1007/978-3-319-73180-3_2
Published Online: 2018-03-29
Published Print: 2018
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Szwaba, Ryszard
Doerffer, Piotr
Kaczynski, Piotr
License valid from 2018-01-01