Experimental Investigation of the Weak Shock Wave Influence on the Boundary Layer of a Flat Blunt Plate at the Mach Number 2.5
Crossref DOI link: https://doi.org/10.1134/S0015462819020058
Published Online: 2019-06-04
Published Print: 2019-03
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Ermolaev, Yu. G.
Kosinov, A. D.
Kocharin, V. L.
Semenov, N. V.
Yatskikh, A. A.
Text and Data Mining valid from 2019-03-01
Version of Record valid from 2019-03-01
Article History
Received: 8 August 2018
Revised: 18 October 2018
Accepted: 18 October 2018
First Online: 4 June 2019