02.3 - Basic Fluid Dynamics and Flow Control
EXPERIMENTAL STUDY OF AEROFOIL-WAKE INDUCED TRANSITION IN BOUNDARY LAYERS
D. Veerasamy, United Kingdom
In this paper an experimental investigation of aerofoil wake induced transition in zero pressure gradient is presented, to gain more specific understanding of the transition onset mechanism and to quantify the shift in transition position, the extent of the transition region and the effect of Reynolds number.