Airfoil: S1223 Builder: Y. Tinel Comment: upper surface vortex generator type "A" @ x/c = 17% Number of Reynolds #'s: 1 Average Reynolds #: 200100 Number of angles of attack: 6 alpha / Cl / Cd / Spanwise Cd's >>> -0.43 0.975 0.0302 0.0300 0.0226 0.0318 0.0363 1.77 1.184 0.0336 0.0345 0.0254 0.0341 0.0404 3.78 1.352 0.0362 0.0386 0.0283 0.0339 0.0440 5.85 1.521 0.0410 0.0453 0.0333 0.0373 0.0481 7.70 1.653 0.0454 0.0514 0.0380 0.0407 0.0516 9.92 1.801 0.0527 0.0618 0.0460 0.0453 0.0575 Tabulated from data in file MS00370.DAT & reduced using program Q01.00L File s1223vg1.drg created on 12-05-1997 at 15:25:59 using program FORMAT