Airfoil: LD-79 Builder: L. DeWitt Comment: clean Number of Reynolds #'s: 4 Average Reynolds #: 59400 Number of angles of attack: 11 alpha / Cl / Cd / Spanwise Cd's >>> -5.60 -0.361 0.0891 0.0981 0.1085 0.0750 0.0750 -4.06 -0.186 0.0491 0.0533 0.0510 0.0457 0.0464 -2.52 0.022 0.0334 0.0348 0.0349 0.0318 0.0320 -1.01 0.197 0.0261 0.0257 0.0260 0.0244 0.0282 0.58 0.450 0.0221 0.0190 0.0247 0.0257 0.0190 2.16 0.618 0.0193 0.0171 0.0175 0.0247 0.0177 3.65 0.763 0.0233 0.0170 0.0197 0.0305 0.0261 5.17 0.899 0.0274 0.0272 0.0210 0.0329 0.0287 6.72 1.036 0.0246 0.0222 0.0218 0.0281 0.0261 8.26 1.130 0.0360 0.0338 0.0328 0.0393 0.0380 9.76 1.191 0.0549 0.0551 0.0529 0.0553 0.0562 Tabulated from data in file FS00945.DAT & reduced using program Q02.00D Average Reynolds #: 99600 Number of angles of attack: 10 alpha / Cl / Cd / Spanwise Cd's >>> -4.58 -0.269 0.0582 0.0584 0.0615 0.0575 0.0556 -3.09 -0.035 0.0391 0.0387 0.0359 0.0417 0.0401 -1.48 0.177 0.0258 0.0285 0.0244 0.0249 0.0256 0.04 0.384 0.0202 0.0197 0.0199 0.0221 0.0191 1.62 0.538 0.0196 0.0183 0.0186 0.0219 0.0196 3.15 0.694 0.0179 0.0162 0.0177 0.0187 0.0190 4.67 0.846 0.0195 0.0185 0.0197 0.0206 0.0190 6.16 0.975 0.0245 0.0234 0.0243 0.0254 0.0249 7.73 1.089 0.0322 0.0308 0.0314 0.0326 0.0341 9.27 1.184 0.0443 0.0421 0.0414 0.0453 0.0483 Tabulated from data in file FS00947.DAT & reduced using program Q02.00D Average Reynolds #: 149400 Number of angles of attack: 9 alpha / Cl / Cd / Spanwise Cd's >>> -4.55 -0.252 0.0572 0.0585 0.0580 0.0561 0.0563 -2.97 -0.029 0.0348 0.0345 0.0333 0.0362 0.0352 -1.51 0.170 0.0239 0.0255 0.0215 0.0241 0.0246 0.12 0.376 0.0190 0.0200 0.0174 0.0191 0.0194 1.59 0.530 0.0174 0.0164 0.0168 0.0185 0.0180 3.16 0.729 0.0160 0.0158 0.0163 0.0162 0.0158 4.63 0.867 0.0179 0.0173 0.0184 0.0178 0.0181 6.23 0.999 0.0264 0.0257 0.0270 0.0258 0.0268 7.75 1.110 0.0344 0.0333 0.0341 0.0345 0.0358 Tabulated from data in file FS00951.DAT & reduced using program Q02.00D Average Reynolds #: 199200 Number of angles of attack: 10 alpha / Cl / Cd / Spanwise Cd's >>> -4.58 -0.264 0.0575 0.0571 0.0560 0.0600 0.0569 -3.33 -0.072 0.0370 0.0370 0.0356 0.0383 0.0371 -1.39 0.187 0.0223 0.0229 0.0207 0.0232 0.0224 0.08 0.394 0.0173 0.0168 0.0173 0.0173 0.0180 1.59 0.556 0.0158 0.0150 0.0166 0.0155 0.0162 3.15 0.719 0.0143 0.0132 0.0152 0.0137 0.0151 6.06 0.982 0.0247 0.0239 0.0249 0.0248 0.0253 6.22 0.990 0.0253 0.0243 0.0256 0.0257 0.0256 7.77 1.102 0.0340 0.0337 0.0333 0.0342 0.0348 9.25 1.178 0.0455 0.0454 0.0438 0.0460 0.0469 Tabulated from data in file FS00949.DAT & reduced using program Q02.00D File ld79.drg created on 09-12-1997 at 13:46:24 using program FORMAT