Airfoil: S823 Builder: M. Allen Comment: Zig-Zag trip type "C" @ x/c = 2% u.s. & 5% l.s. (h/c = 0.19%) Number of Reynolds #'s: 4 Average Reynolds #: 100700 Number of angles of attack: 10 alpha / Cl / Cd / Spanwise Cd's >>> -2.79 -0.197 0.0375 0.0377 0.0351 0.0394 0.0375 -1.22 -0.006 0.0379 0.0378 0.0377 0.0389 0.0371 0.31 0.169 0.0384 0.0374 0.0374 0.0404 0.0382 1.84 0.385 0.0298 0.0295 0.0342 0.0281 0.0276 3.39 0.564 0.0231 0.0240 0.0217 0.0237 0.0230 4.92 0.713 0.0233 0.0232 0.0228 0.0230 0.0243 6.43 0.805 0.0269 0.0259 0.0264 0.0275 0.0276 7.97 0.888 0.0317 0.0310 0.0312 0.0329 0.0315 9.48 0.957 0.0364 0.0362 0.0370 0.0372 0.0353 10.99 1.004 0.0456 0.0476 0.0494 0.0422 0.0432 Tabulated from data in file CL00730.DAT & reduced using program Q02.00D Average Reynolds #: 201300 Number of angles of attack: 11 alpha / Cl / Cd / Spanwise Cd's >>> -3.69 -0.111 0.0259 0.0255 0.0239 0.0293 0.0248 -2.25 0.001 0.0234 0.0231 0.0223 0.0254 0.0230 -0.71 0.154 0.0212 0.0194 0.0246 0.0209 0.0200 0.81 0.303 0.0193 0.0187 0.0198 0.0191 0.0197 2.36 0.440 0.0204 0.0203 0.0191 0.0205 0.0216 3.91 0.574 0.0223 0.0221 0.0218 0.0224 0.0230 5.41 0.699 0.0244 0.0236 0.0242 0.0248 0.0250 6.96 0.811 0.0280 0.0277 0.0281 0.0278 0.0286 8.47 0.904 0.0331 0.0325 0.0342 0.0331 0.0326 9.97 0.969 0.0443 0.0455 0.0421 0.0430 0.0467 11.49 1.017 0.0649 0.0737 0.0689 0.0548 0.0623 Tabulated from data in file PG00834.DAT & reduced using program Q02.00D Average Reynolds #: 301900 Number of angles of attack: 10 alpha / Cl / Cd / Spanwise Cd's >>> -2.74 -0.052 0.0212 0.0211 0.0205 0.0238 0.0192 -1.23 0.086 0.0186 0.0194 0.0181 0.0191 0.0179 0.31 0.237 0.0180 0.0180 0.0167 0.0184 0.0187 1.81 0.371 0.0195 0.0197 0.0186 0.0195 0.0204 3.37 0.519 0.0209 0.0206 0.0206 0.0207 0.0217 4.84 0.646 0.0227 0.0223 0.0224 0.0225 0.0235 6.43 0.767 0.0254 0.0255 0.0250 0.0250 0.0262 7.80 0.855 0.0293 0.0289 0.0284 0.0286 0.0312 9.47 0.936 0.0380 0.0369 0.0354 0.0395 0.0404 10.93 0.989 0.0531 0.0514 0.0518 0.0579 0.0514 Tabulated from data in file PG00836.DAT & reduced using program Q02.00D Average Reynolds #: 402800 Number of angles of attack: 10 alpha / Cl / Cd / Spanwise Cd's >>> -2.75 -0.054 0.0196 0.0206 0.0180 0.0206 0.0191 -1.22 0.090 0.0183 0.0193 0.0172 0.0188 0.0178 0.41 0.244 0.0185 0.0192 0.0179 0.0189 0.0181 1.85 0.401 0.0193 0.0194 0.0188 0.0197 0.0193 3.37 0.547 0.0203 0.0203 0.0202 0.0202 0.0207 5.01 0.692 0.0222 0.0219 0.0221 0.0217 0.0230 6.44 0.791 0.0247 0.0243 0.0247 0.0241 0.0258 7.95 0.877 0.0291 0.0286 0.0286 0.0282 0.0310 9.80 0.960 0.0404 0.0389 0.0361 0.0433 0.0433 11.01 0.999 0.0484 0.0429 0.0492 0.0621 0.0393 Tabulated from data in file PG00733.DAT & reduced using program Q02.00D File s823t.drg created on 09-12-1997 at 13:46:24 using program FORMAT