XFOIL Version 6.96 Calculated polar for: FX 78-PK-188/20 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.000 -0.4845 0.09388 0.08918 -0.0985 0.8089 0.0168 -15.750 -0.5212 0.08275 0.07785 -0.1053 0.8080 0.0167 -15.500 -0.5469 0.07502 0.06992 -0.1097 0.8068 0.0166 -15.250 -0.5669 0.06900 0.06373 -0.1127 0.8052 0.0165 -15.000 -0.5931 0.06284 0.05729 -0.1150 0.8034 0.0167 -14.750 -0.6145 0.05791 0.05209 -0.1161 0.8014 0.0168 -14.500 -0.6274 0.05423 0.04821 -0.1163 0.7994 0.0170 -14.250 -0.6326 0.05156 0.04542 -0.1161 0.7974 0.0172 -14.000 -0.6364 0.04913 0.04285 -0.1157 0.7956 0.0174 -13.750 -0.6370 0.04717 0.04077 -0.1151 0.7939 0.0177 -13.500 -0.6369 0.04532 0.03878 -0.1144 0.7924 0.0181 -13.250 -0.6367 0.04341 0.03670 -0.1134 0.7909 0.0184 -13.000 -0.6347 0.04172 0.03488 -0.1124 0.7892 0.0190 -12.750 -0.6315 0.03991 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