XFOIL Version 6.96 Calculated polar for: MH 46 9.1% 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -5.500 -0.4825 0.01413 0.00914 -0.0189 0.9002 0.0049 -5.250 -0.4594 0.01311 0.00798 -0.0178 0.8859 0.0047 -5.000 -0.4374 0.01177 0.00644 -0.0164 0.8724 0.0045 -4.750 -0.4138 0.01089 0.00538 -0.0154 0.8596 0.0045 -4.500 -0.3892 0.01019 0.00454 -0.0145 0.8474 0.0045 -4.250 -0.3638 0.00967 0.00389 -0.0139 0.8356 0.0045 -4.000 -0.3378 0.00926 0.00335 -0.0133 0.8244 0.0047 -3.750 -0.3116 0.00887 0.00284 -0.0127 0.8135 0.0050 -3.500 -0.2854 0.00850 0.00234 -0.0122 0.8028 0.0075 -3.250 -0.2603 0.00790 0.00195 -0.0116 0.7921 0.0567 -3.000 -0.2343 0.00754 0.00175 -0.0112 0.7817 0.1001 -2.750 -0.2083 0.00721 0.00158 -0.0109 0.7717 0.1520 -2.500 -0.1828 0.00683 0.00143 -0.0105 0.7616 0.2227 -2.250 -0.1567 0.00653 0.00131 -0.0102 0.7513 0.2839 -2.000 -0.1300 0.00633 0.00121 -0.0100 0.7413 0.3300 -1.750 -0.1035 0.00612 0.00112 -0.0097 0.7313 0.3811 -1.500 -0.0774 0.00589 0.00105 -0.0093 0.7209 0.4430 -1.250 -0.0507 0.00573 0.00100 -0.0090 0.7101 0.4888 -1.000 -0.0243 0.00556 0.00094 -0.0087 0.6993 0.5414 -0.750 0.0018 0.00539 0.00090 -0.0083 0.6883 0.5951 -0.500 0.0273 0.00520 0.00087 -0.0077 0.6769 0.6555 -0.250 0.0517 0.00498 0.00084 -0.0069 0.6649 0.7287 0.000 0.0746 0.00470 0.00083 -0.0056 0.6523 0.8170 0.250 0.1048 0.00445 0.00085 -0.0058 0.6389 0.9168 0.500 0.1698 0.00452 0.00090 -0.0139 0.6217 0.9604 0.750 0.2094 0.00463 0.00094 -0.0164 0.6046 0.9766 1.000 0.2451 0.00475 0.00098 -0.0180 0.5870 0.9875 2.000 0.3838 0.00516 0.00107 -0.0241 0.5085 1.0000 2.250 0.4096 0.00526 0.00110 -0.0237 0.4888 1.0000 2.500 0.4354 0.00538 0.00115 -0.0233 0.4696 1.0000 2.750 0.4614 0.00550 0.00121 -0.0228 0.4505 1.0000 3.250 0.5131 0.00578 0.00136 -0.0221 0.4108 1.0000 3.750 0.5648 0.00612 0.00156 -0.0213 0.3672 1.0000 4.000 0.5905 0.00631 0.00167 -0.0209 0.3457 1.0000 4.250 0.6161 0.00653 0.00181 -0.0205 0.3208 1.0000 4.500 0.6416 0.00676 0.00197 -0.0201 0.2948 1.0000 4.750 0.6669 0.00704 0.00213 -0.0197 0.2669 1.0000 5.000 0.6920 0.00732 0.00232 -0.0193 0.2399 1.0000 5.250 0.7171 0.00763 0.00253 -0.0189 0.2132 1.0000 5.500 0.7417 0.00800 0.00277 -0.0184 0.1833 1.0000 5.750 0.7663 0.00837 0.00304 -0.0180 0.1563 1.0000 6.000 0.7908 0.00875 0.00332 -0.0175 0.1306 1.0000 6.250 0.8150 0.00916 0.00362 -0.0170 0.1064 1.0000 6.500 0.8392 0.00956 0.00394 -0.0165 0.0860 1.0000 6.750 0.8629 0.01002 0.00430 -0.0159 0.0660 1.0000 7.000 0.8867 0.01046 0.00467 -0.0153 0.0498 1.0000 7.250 0.9097 0.01099 0.00511 -0.0147 0.0345 1.0000 7.500 0.9329 0.01148 0.00558 -0.0140 0.0245 1.0000 7.750 0.9565 0.01192 0.00603 -0.0134 0.0189 1.0000 8.000 0.9791 0.01247 0.00656 -0.0126 0.0145 1.0000 8.250 1.0024 0.01290 0.00705 -0.0119 0.0128 1.0000 8.500 1.0259 0.01328 0.00746 -0.0113 0.0112 1.0000 8.750 1.0478 0.01387 0.00806 -0.0105 0.0090 1.0000 9.000 1.0701 0.01438 0.00863 -0.0098 0.0074 1.0000 9.250 1.0891 0.01531 0.00960 -0.0086 0.0046 1.0000 9.500 1.1108 0.01584 0.01021 -0.0078 0.0037 1.0000 9.750 1.1308 0.01655 0.01098 -0.0067 0.0032 1.0000 10.000 1.1469 0.01768 0.01224 -0.0052 0.0028 1.0000 10.250 1.1601 0.01904 0.01376 -0.0034 0.0026 1.0000 10.500 1.1719 0.02044 0.01533 -0.0014 0.0024 1.0000 10.750 1.1899 0.02112 0.01609 -0.0003 0.0024 1.0000 11.000 1.2036 0.02216 0.01723 0.0013 0.0023 1.0000 11.250 1.2179 0.02305 0.01822 0.0028 0.0022 1.0000 11.500 1.2281 0.02420 0.01948 0.0047 0.0021 1.0000 11.750 1.2284 0.02565 0.02108 0.0079 0.0021 1.0000 12.000 1.2296 0.02715 0.02270 0.0104 0.0021 1.0000 12.250 1.2295 0.02904 0.02474 0.0121 0.0020 1.0000 12.500 1.2306 0.03107 0.02693 0.0132 0.0020 1.0000 12.750 1.2268 0.03381 0.02984 0.0139 0.0020 1.0000 13.000 1.2197 0.03720 0.03341 0.0139 0.0020 1.0000 13.250 1.2146 0.04063 0.03700 0.0133 0.0020 1.0000 13.500 1.2056 0.04480 0.04134 0.0121 0.0020 1.0000 13.750 1.2083 0.04765 0.04428 0.0109 0.0019 1.0000 14.000 1.1943 0.05300 0.04981 0.0086 0.0019 1.0000 14.250 1.1791 0.05890 0.05588 0.0058 0.0019 1.0000 14.500 1.1670 0.06459 0.06170 0.0028 0.0019 1.0000 14.750 1.1446 0.07220 0.06949 -0.0012 0.0020 1.0000 15.000 1.1294 0.07898 0.07639 -0.0049 0.0019 1.0000 15.250 1.1104 0.08670 0.08424 -0.0090 0.0019 1.0000 15.500 1.0830 0.09635 0.09404 -0.0140 0.0020 1.0000