Airfoil: SG6041 Builder: M. Allen Comment: Zigzag trip Type C (h = 0.023") @ 2% u.s. & 5% l.s. Number of Reynolds #'s: 3 Average Reynolds #: 144195 Number of angles of attack: 13 alpha / Cl / Cd / Spanwise Cd's >>> -5.68 -0.401 0.0363 0.0368 0.0360 0.0354 0.0369 -4.36 -0.297 0.0231 0.0236 0.0226 0.0233 0.0229 -2.86 -0.151 0.0173 0.0172 0.0193 0.0159 0.0167 -1.24 0.102 0.0170 0.0173 0.0163 0.0171 0.0174 0.29 0.289 0.0139 0.0136 0.0139 0.0141 0.0140 1.88 0.413 0.0169 0.0168 0.0168 0.0169 0.0172 3.28 0.529 0.0177 0.0178 0.0185 0.0168 0.0176 5.00 0.675 0.0205 0.0205 0.0210 0.0202 0.0205 6.38 0.802 0.0241 0.0244 0.0248 0.0238 0.0234 7.87 0.917 0.0287 0.0293 0.0291 0.0283 0.0281 9.53 1.008 0.0366 0.0373 0.0366 0.0359 0.0366 10.92 1.071 0.0449 0.0447 0.0446 0.0455 0.0448 6.00 0.925 0.0128 0.1918 0.2046 0.0128 0.0124 Tabulated from data in file pg02528.dat & reduced using program C06.01 Average Reynolds #: 299200 Number of angles of attack: 13 alpha / Cl / Cd / Spanwise Cd's >>> -5.85 -0.408 0.0346 0.0382 0.0351 0.0321 0.0331 -4.30 -0.217 0.0167 0.0181 0.0157 0.0154 0.0175 -2.84 -0.018 0.0120 0.0126 0.0129 0.0109 0.0115 -1.21 0.131 0.0135 0.0135 0.0135 0.0134 0.0136 0.44 0.296 0.0148 0.0151 0.0148 0.0146 0.0147 1.94 0.456 0.0162 0.0164 0.0163 0.0160 0.0161 3.39 0.598 0.0180 0.0181 0.0184 0.0177 0.0177 4.89 0.736 0.0206 0.0205 0.0212 0.0203 0.0203 6.39 0.867 0.0236 0.0238 0.0239 0.0235 0.0231 8.08 0.987 0.0282 0.0283 0.0291 0.0272 0.0284 9.41 1.064 0.0340 0.0341 0.0344 0.0331 0.0343 10.90 1.121 0.0439 0.0427 0.0431 0.0421 0.0476 12.35 1.138 0.0674 0.0540 0.0496 0.0666 0.0996 Tabulated from data in file pg02531.dat & reduced using program C06.01 Average Reynolds #: 498804 Number of angles of attack: 13 alpha / Cl / Cd / Spanwise Cd's >>> -5.87 -0.333 0.0205 0.0211 0.0209 0.0199 0.0203 -4.31 -0.175 0.0148 0.0147 0.0148 0.0144 0.0154 -2.72 -0.017 0.0128 0.0130 0.0129 0.0122 0.0132 -1.46 0.127 0.0132 0.0132 0.0132 0.0130 0.0134 0.22 0.306 0.0138 0.0138 0.0136 0.0139 0.0137 1.71 0.465 0.0150 0.0151 0.0149 0.0150 0.0149 3.34 0.628 0.0169 0.0171 0.0171 0.0169 0.0166 4.86 0.769 0.0195 0.0197 0.0197 0.0196 0.0191 6.60 0.923 0.0236 0.0236 0.0242 0.0233 0.0235 8.03 1.025 0.0277 0.0274 0.0280 0.0279 0.0276 9.59 1.103 0.0333 0.0314 0.0333 0.0340 0.0343 10.87 1.143 0.0372 0.0330 0.0371 0.0396 0.0389 12.54 1.184 0.0383 0.0375 0.0378 0.0394 0.0386 Tabulated from data in file pg02534.dat & reduced using program C06.01 File sg6041t.drg created using program C06.01 on Mon Feb 02 15:11:43 1998