Airfoil: FX 74-CL5-140 MOD Builder: C. Hollinger Comment: clean Number of Reynolds #'s: 1 Average Reynolds #: 199400 Number of angles of attack: 9 alpha / Cl / Cd / Spanwise Cd's >>> -1.80 0.611 0.0379 0.0367 0.0377 0.0390 0.0380 -0.47 0.859 0.0258 0.0251 0.0248 0.0277 0.0254 1.20 1.049 0.0223 0.0217 0.0213 0.0245 0.0218 2.71 1.200 0.0211 0.0209 0.0208 0.0221 0.0206 4.25 1.347 0.0234 0.0232 0.0227 0.0250 0.0228 5.60 1.468 0.0253 0.0250 0.0248 0.0264 0.0251 7.42 1.622 0.0285 0.0278 0.0285 0.0295 0.0283 9.05 1.749 0.0318 0.0310 0.0320 0.0328 0.0316 10.48 1.850 0.0351 0.0349 0.0353 0.0356 0.0345 Tabulated from data in file AB00185.DAT & reduced using program Q01.00L File fx74mod.drg created on 12-05-1997 at 15:25:58 using program FORMAT