![](/img/cover-not-exists.png)
Experimental Investigation of the Weak Shock Wave Influence on the Boundary Layer of a Flat Blunt Plate at the Mach Number 2.5
Ermolaev, Yu. G., Kosinov, A. D., Kocharin, V. L., Semenov, N. V., Yatskikh, A. A.Volume:
54
Language:
english
Journal:
Fluid Dynamics
DOI:
10.1134/S0015462819020058
Date:
March, 2019
File:
PDF, 525 KB
english, 2019