Impact of incident Mach wave on supersonic boundary layer

Research output: Contribution to journal › Article › peer-review

Original language	English
Pages (from-to)	43-48
Number of pages	6
Journal	Thermophysics and Aeromechanics
Volume	23
Issue number	1
DOIs	https://doi.org/10.1134/S0869864316010054
Publication status	Published - 1 Jan 2016

boundary layer, experimental studies, flat plate, hot-wire anemometry, sharp and blunt leading edges, supersonic velocities, wind tunnel

ID: 25840502