Experimental study of the action of weak shock waves on the boundary layer flow on a swept flat plate at the Mach number 2
Year: 2024
Type: article
Source: Thermophysics and Aeromechanics
Institution: Institute of Theoretical and Applied Mechanics
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4405370030
