论文信息 - Flow visualization studies of the Mach number effects on the dynamic stall of an oscillating airfoil

Flow visualization studies of the Mach number effects on the dynamic stall of an oscillating airfoil

Compressibility effects on dynamic stall of a NACA 0012 airfoil undergoing sinusoidal oscillatory motion were studied using a stroboscopic schlieren system. Schlieren pictures and some quantitative data derived from the are presented and show the influence of freestream Mach number and reduced frequency on the dynamic stall vortex

M. S. Chandrasekhara | L. W. Carr | L. Carr | M. Chandrasekhara

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