Airfoil: SG6042 Builder: M. Allen Comment: Zigzag trip Type C (h = 0.023") @ 2% u.s. & 5% l.s. (Cm @ 500,000 is incorrect) Number of Reynolds #'s: 5 Average Reynolds #: 149755 Number of angles of attack: 13 alpha / Cl / Cd / Spanwise Cd's >>> -6.25 -0.422 0.0914 0.0932 0.0901 0.0889 0.0934 -4.44 -0.177 0.0356 0.0362 0.0346 0.0350 0.0366 -2.81 0.053 0.0219 0.0213 0.0221 0.0215 0.0229 -1.30 0.246 0.0224 0.0224 0.0228 0.0223 0.0219 0.33 0.476 0.0144 0.0149 0.0153 0.0141 0.0131 1.91 0.602 0.0177 0.0173 0.0187 0.0172 0.0177 3.12 0.695 0.0197 0.0197 0.0196 0.0196 0.0197 4.91 0.833 0.0215 0.0213 0.0218 0.0217 0.0212 6.40 0.952 0.0254 0.0255 0.0253 0.0254 0.0256 7.87 1.059 0.0299 0.0308 0.0301 0.0296 0.0292 9.43 1.147 0.0368 0.0371 0.0368 0.0363 0.0369 10.85 1.199 0.0470 0.0499 0.0441 0.0480 0.0461 12.36 1.231 0.0602 0.0623 0.0595 0.0603 0.0587 Tabulated from data in file pg02549.dat & reduced using program C06.01 Average Reynolds #: 299566 Number of angles of attack: 13 alpha / Cl / Cd / Spanwise Cd's >>> -6.14 -0.279 0.0699 0.0719 0.0681 0.0689 0.0707 -4.50 -0.005 0.0175 0.0158 0.0176 0.0179 0.0189 -2.79 0.175 0.0125 0.0118 0.0119 0.0147 0.0116 -1.32 0.308 0.0135 0.0143 0.0131 0.0129 0.0136 0.07 0.443 0.0148 0.0147 0.0149 0.0145 0.0151 1.71 0.602 0.0168 0.0169 0.0170 0.0166 0.0169 3.41 0.761 0.0191 0.0191 0.0197 0.0187 0.0189 4.56 0.860 0.0207 0.0207 0.0213 0.0203 0.0206 6.69 1.036 0.0252 0.0255 0.0255 0.0244 0.0255 8.11 1.128 0.0293 0.0295 0.0295 0.0278 0.0303 9.19 1.187 0.0340 0.0349 0.0343 0.0311 0.0356 10.77 1.240 0.0436 0.0452 0.0426 0.0401 0.0463 12.38 1.267 0.0624 0.0683 0.0512 0.0484 0.0817 Tabulated from data in file pg02552.dat & reduced using program C06.01 Average Reynolds #: 298975 Number of angles of attack: 2 alpha / Cl / Cd / Spanwise Cd's >>> -5.37 -0.133 0.0420 0.0431 0.0405 0.0404 0.0439 -3.76 0.090 0.0140 0.0114 0.0143 0.0149 0.0154 Tabulated from data in file pg02553.dat & reduced using program C06.01 Average Reynolds #: 499026 Number of angles of attack: 11 alpha / Cl / Cd / Spanwise Cd's >>> -4.46 -0.003 0.0157 0.0157 0.0155 0.0156 0.0161 -3.00 0.148 0.0136 0.0139 0.0135 0.0132 0.0140 -1.31 0.319 0.0135 0.0134 0.0133 0.0136 0.0136 -0.05 0.445 0.0141 0.0141 0.0140 0.0141 0.0143 1.60 0.614 0.0155 0.0157 0.0155 0.0155 0.0155 3.31 0.779 0.0176 0.0179 0.0181 0.0172 0.0172 4.71 0.904 0.0198 0.0198 0.0202 0.0195 0.0197 6.10 1.020 0.0225 0.0226 0.0229 0.0222 0.0224 7.79 1.141 0.0272 0.0273 0.0279 0.0265 0.0274 9.47 1.228 0.0333 0.0332 0.0334 0.0330 0.0335 10.96 1.278 0.0416 0.0425 0.0387 0.0424 0.0429 Tabulated from data in file pg02556.dat & reduced using program C06.01 Average Reynolds #: 500070 Number of angles of attack: 2 alpha / Cl / Cd / Spanwise Cd's >>> -5.60 -0.120 0.0402 0.0407 0.0399 0.0392 0.0409 -5.02 -0.051 0.0173 0.0179 0.0170 0.0160 0.0184 Tabulated from data in file pg02557.dat & reduced using program C06.01 File sg6042t.drg created using program C06.01 on Mon Feb 02 15:11:43 1998