Reynolds number influence on the backpressure-induced shock–boundary layer interaction in an asymmetric supersonic expansion flow
Crossref DOI link: https://doi.org/10.1007/s42401-019-00025-x
Published Online: 2019-04-17
Published Print: 2019-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Ji, Yuan
He, Miaosheng http://orcid.org/0000-0002-5103-9955
Liu, Hong
Funding for this research was provided by:
Major Research Plan (91441205)
Text and Data Mining valid from 2019-04-17
Article History
Received: 15 January 2019
Revised: 31 March 2019
Accepted: 4 April 2019
First Online: 17 April 2019