1. Instantaneous streamlines are presented in the reference frame attached to the airfoil. In such reference frame,forward (or reversed)flow is defined as the flow moving from the leading edge to the trailing edge (or from the trailing edge to the leading edge). The instantaneous stream lines for the entire airfoil and the vicinity of the leading edge at four different angles of attack (a= 16.5', a = 24O, a = 27' and a = 30") are shownin Fig. 8-14.
2. No. of Processors CPUTimex(lo-') rteocell 0) breaks down at early stage of the airfoil
3. AIAA Paper, Paper No-89-0115,1989.