Effect of Reynolds number on a normal shock wave-transitional boundary-layer interaction over a curved surface
Crossref DOI link: https://doi.org/10.1007/s00348-019-2824-0
Published Online: 2019-11-13
Published Print: 2019-12
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Coschignano, A. http://orcid.org/0000-0002-0531-8347
Atkins, N.
Babinsky, H.
Serna, J.
Funding for this research was provided by:
Rolls-Royce
Text and Data Mining valid from 2019-11-13
Version of Record valid from 2019-11-13
Article History
Received: 12 August 2019
Revised: 9 October 2019
Accepted: 10 October 2019
First Online: 13 November 2019