03.2 - Experimental Aerodynamics
EFFECT OF FREESTREAM DISTURBANCES ON BOUNDARY LAYER TRANSITION IN HYPERSONIC WIND TUNNEL
J. Yuan¹, S. Yu¹, Z. Qian¹; ¹AVIC Aerodynamics Research Institute, China
The effect of freestream disturbances on hypersonic boundary layer transition is studied based on two hypersonic wind tunnels in AVIC Aerodynamics Research Institute