Zobrazeno 1 - 3
of 3
pro vyhledávání: '"I. M. Ilyukhin"'
Publikováno v:
Fluid Dynamics. 55:681-688
The results of numerical simulation of the interaction between a shock and the laminar boundary layer on a flat plate in motion in supersonic perfect-gas flow at Mach number М∞ = 3 are considered. The shock is preassigned using the Rankine—Hugon
Publikováno v:
AIP Conference Proceedings.
Publikováno v:
AIP Conference Proceedings.
The results of numerical simulation of the interaction between a shock and the laminar boundary layer on a flat plate in motion in supersonic perfect-gas flow at Mach numbers M∞ = 2.3 and M∞ = 3 are considered. The shock is preassigned using the