Visualization of curved swept shock wave/turbulent boundary layer interaction in supersonic flow
Crossref DOI link: https://doi.org/10.1007/s12650-020-00692-5
Published Online: 2020-09-02
Published Print: 2021-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zhang, Yue
Chen, Liang
Tan, Hui-jun
Wang, Chao
Cheng, Fei
Li, Chao
Text and Data Mining valid from 2020-09-02
Version of Record valid from 2020-09-02
Article History
Received: 15 April 2020
Revised: 30 June 2020
Accepted: 10 August 2020
First Online: 2 September 2020