Numerical Simulation of Shock Wave Turbulent Boundary Layer Interaction over Flat Plate at Mach 6
Crossref DOI link: https://doi.org/10.1007/s40032-021-00732-5
Published Online: 2021-06-29
Published Print: 2024-08
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Mehta, R. C.
Text and Data Mining valid from 2021-06-29
Version of Record valid from 2021-06-29
Article History
Received: 11 February 2021
Accepted: 22 June 2021
First Online: 29 June 2021