XFOIL Version 6.96 Calculated polar for: RONCZ 1080 VOYAGER INNER AFT WING AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -12.250 -0.2390 0.08857 0.08488 -0.1008 0.7113 0.0296 -12.000 -0.5706 0.03797 0.03269 -0.1122 0.7165 0.0159 -11.750 -0.5773 0.03569 0.03023 -0.1097 0.7127 0.0158 -11.500 -0.5848 0.03353 0.02781 -0.1066 0.7091 0.0158 -11.250 -0.5867 0.03159 0.02562 -0.1038 0.7059 0.0158 -11.000 -0.5831 0.02983 0.02363 -0.1014 0.7027 0.0156 -10.750 -0.5779 0.02830 0.02189 -0.0989 0.7000 0.0158 -10.500 -0.5694 0.02704 0.02044 -0.0966 0.6972 0.0160 -10.250 -0.5573 0.02569 0.01889 -0.0948 0.6945 0.0161 -10.000 -0.5424 0.02459 0.01763 -0.0932 0.6920 0.0162 -9.750 -0.5251 0.02362 0.01650 -0.0920 0.6896 0.0163 -9.500 -0.5090 0.02289 0.01559 -0.0904 0.6873 0.0164 -9.250 -0.4816 0.02149 0.01409 -0.0909 0.6851 0.0166 -9.000 -0.4591 0.02044 0.01305 -0.0906 0.6833 0.0172 -8.750 -0.4399 0.01981 0.01240 -0.0896 0.6813 0.0176 -8.500 -0.4205 0.01923 0.01178 -0.0885 0.6793 0.0181 -8.250 -0.4012 0.01865 0.01114 -0.0874 0.6772 0.0186 -8.000 -0.3823 0.01811 0.01053 -0.0861 0.6752 0.0193 -7.750 -0.3640 0.01759 0.00994 -0.0847 0.6733 0.0195 -7.500 -0.3476 0.01700 0.00931 -0.0830 0.6717 0.0200 -7.250 -0.3333 0.01643 0.00872 -0.0810 0.6700 0.0208 -7.000 -0.3155 0.01608 0.00834 -0.0795 0.6682 0.0216 -6.750 -0.2965 0.01568 0.00792 -0.0781 0.6670 0.0226 -6.500 -0.2772 0.01530 0.00751 -0.0768 0.6657 0.0237 -6.250 -0.2590 0.01484 0.00707 -0.0753 0.6643 0.0253 -6.000 -0.2382 0.01453 0.00673 -0.0743 0.6628 0.0273 -5.750 -0.2181 0.01416 0.00637 -0.0731 0.6614 0.0313 -5.500 -0.1985 0.01374 0.00601 -0.0718 0.6600 0.0398 -5.250 -0.1800 0.01327 0.00568 -0.0703 0.6587 0.0632 -5.000 -0.1595 0.01292 0.00545 -0.0693 0.6574 0.0904 -4.750 -0.1382 0.01261 0.00525 -0.0684 0.6560 0.1184 -4.500 -0.1170 0.01230 0.00506 -0.0674 0.6546 0.1523 -4.250 -0.0972 0.01193 0.00488 -0.0663 0.6533 0.2020 -4.000 -0.0786 0.01152 0.00474 -0.0651 0.6520 0.2700 -3.750 -0.0630 0.01096 0.00457 -0.0633 0.6508 0.3671 -3.500 -0.0530 0.01008 0.00431 -0.0605 0.6499 0.5129 -3.250 -0.0402 0.00953 0.00445 -0.0576 0.6489 0.6702 -3.000 -0.0143 0.00969 0.00466 -0.0570 0.6479 0.7141 -2.750 0.0130 0.00987 0.00482 -0.0568 0.6468 0.7326 -2.500 0.0403 0.01005 0.00496 -0.0567 0.6456 0.7463 -2.250 0.0684 0.01025 0.00515 -0.0566 0.6445 0.7556 -2.000 0.0960 0.01039 0.00524 -0.0565 0.6432 0.7640 -1.750 0.1244 0.01058 0.00542 -0.0565 0.6419 0.7708 -1.500 0.1521 0.01073 0.00552 -0.0565 0.6408 0.7784 -1.250 0.1804 0.01089 0.00567 -0.0565 0.6397 0.7837 -1.000 0.2085 0.01110 0.00588 -0.0564 0.6387 0.7903 -0.750 0.2361 0.01131 0.00605 -0.0563 0.6378 0.7984 -0.500 0.2640 0.01158 0.00633 -0.0560 0.6367 0.8045 -0.250 0.2919 0.01182 0.00654 -0.0560 0.6355 0.8110 0.000 0.3193 0.01204 0.00673 -0.0561 0.6341 0.8157 0.250 0.3461 0.01213 0.00685 -0.0559 0.6333 0.8187 0.500 0.3732 0.01220 0.00693 -0.0559 0.6322 0.8214 0.750 0.4004 0.01225 0.00699 -0.0560 0.6309 0.8239 1.000 0.4277 0.01230 0.00704 -0.0562 0.6295 0.8265 1.250 0.4552 0.01234 0.00708 -0.0564 0.6281 0.8289 1.500 0.4832 0.01239 0.00711 -0.0568 0.6265 0.8310 1.750 0.5104 0.01238 0.00711 -0.0569 0.6250 0.8327 2.000 0.5382 0.01238 0.00712 -0.0571 0.6234 0.8342 2.250 0.5665 0.01240 0.00713 -0.0574 0.6219 0.8357 2.500 0.5953 0.01244 0.00715 -0.0578 0.6204 0.8374 2.750 0.6245 0.01252 0.00721 -0.0584 0.6188 0.8389 3.000 0.6525 0.01270 0.00738 -0.0588 0.6170 0.8406 3.250 0.6785 0.01268 0.00742 -0.0587 0.6151 0.8426 3.500 0.7050 0.01268 0.00745 -0.0588 0.6126 0.8443 3.750 0.7323 0.01265 0.00745 -0.0590 0.6100 0.8458 4.000 0.7604 0.01262 0.00741 -0.0593 0.6074 0.8475 4.250 0.7898 0.01253 0.00731 -0.0599 0.6050 0.8488 4.500 0.8202 0.01246 0.00722 -0.0606 0.6025 0.8499 4.750 0.8473 0.01248 0.00726 -0.0607 0.5995 0.8512 5.000 0.8713 0.01240 0.00727 -0.0602 0.5959 0.8526 5.250 0.8975 0.01231 0.00722 -0.0601 0.5923 0.8541 5.500 0.9260 0.01219 0.00710 -0.0604 0.5889 0.8558 5.750 0.9562 0.01212 0.00701 -0.0610 0.5860 0.8575 6.000 0.9813 0.01210 0.00705 -0.0608 0.5823 0.8592 6.250 1.0051 0.01202 0.00705 -0.0603 0.5779 0.8610 6.500 1.0321 0.01190 0.00695 -0.0603 0.5735 0.8626 6.750 1.0610 0.01178 0.00680 -0.0608 0.5694 0.8641 7.000 1.0829 0.01172 0.00684 -0.0599 0.5643 0.8658 7.250 1.1054 0.01158 0.00678 -0.0590 0.5583 0.8676 7.500 1.1309 0.01146 0.00665 -0.0587 0.5527 0.8695 7.750 1.1483 0.01141 0.00673 -0.0569 0.5445 0.8722 8.000 1.1700 0.01133 0.00667 -0.0559 0.5369 0.8746 8.250 1.1877 0.01132 0.00676 -0.0543 0.5259 0.8772 8.500 1.2042 0.01135 0.00681 -0.0524 0.5124 0.8799 8.750 1.2134 0.01139 0.00685 -0.0490 0.4946 0.8830 9.000 1.2142 0.01163 0.00704 -0.0441 0.4704 0.8870 9.250 1.2075 0.01222 0.00752 -0.0382 0.4433 0.8924 9.500 1.1986 0.01307 0.00825 -0.0325 0.4180 0.8985 9.750 1.1874 0.01407 0.00921 -0.0267 0.3942 0.9062 10.000 1.1758 0.01536 0.01045 -0.0216 0.3717 0.9154 10.250 1.1644 0.01684 0.01190 -0.0169 0.3503 0.9280 10.500 1.1594 0.01857 0.01362 -0.0140 0.3265 0.9483 10.750 1.1730 0.02088 0.01587 -0.0162 0.2976 0.9806 11.000 1.1696 0.02286 0.01775 -0.0142 0.2775 1.0000 11.250 1.1669 0.02484 0.01964 -0.0123 0.2590 1.0000 11.500 1.1655 0.02675 0.02146 -0.0105 0.2414 1.0000 11.750 1.1654 0.02859 0.02323 -0.0089 0.2244 1.0000 12.000 1.1663 0.03041 0.02498 -0.0074 0.2090 1.0000 12.250 1.1682 0.03220 0.02672 -0.0060 0.1945 1.0000 12.500 1.1709 0.03398 0.02843 -0.0048 0.1808 1.0000 12.750 1.1746 0.03573 0.03013 -0.0037 0.1677 1.0000 13.000 1.1797 0.03739 0.03176 -0.0027 0.1554 1.0000 13.250 1.1850 0.03908 0.03342 -0.0018 0.1444 1.0000 13.500 1.1900 0.04084 0.03514 -0.0010 0.1342 1.0000 13.750 1.1939 0.04270 0.03696 -0.0001 0.1241 1.0000 14.000 1.2002 0.04442 0.03865 0.0005 0.1149 1.0000 14.250 1.2065 0.04615 0.04037 0.0011 0.1065 1.0000 14.500 1.2101 0.04817 0.04234 0.0018 0.0982 1.0000 14.750 1.2171 0.04991 0.04408 0.0022 0.0910 1.0000 15.000 1.2229 0.05177 0.04595 0.0027 0.0852 1.0000 15.250 1.2288 0.05368 0.04786 0.0030 0.0797 1.0000 15.500 1.2336 0.05572 0.04991 0.0034 0.0751 1.0000 15.750 1.2416 0.05750 0.05173 0.0036 0.0713 1.0000 16.000 1.2448 0.05977 0.05400 0.0038 0.0675 1.0000 16.250 1.2512 0.06175 0.05603 0.0040 0.0644 1.0000 16.500 1.2576 0.06377 0.05810 0.0040 0.0614 1.0000 16.750 1.2602 0.06623 0.06056 0.0041 0.0584 1.0000 17.000 1.2654 0.06845 0.06284 0.0040 0.0559 1.0000 17.250 1.2711 0.07065 0.06511 0.0039 0.0536 1.0000 17.500 1.2745 0.07312 0.06760 0.0037 0.0510 1.0000 17.750 1.2747 0.07601 0.07053 0.0035 0.0487 1.0000 18.000 1.2818 0.07816 0.07277 0.0031 0.0466 1.0000 18.250 1.2845 0.08086 0.07552 0.0027 0.0446 1.0000 18.500 1.2835 0.08405 0.07872 0.0022 0.0425 1.0000 18.750 1.2867 0.08678 0.08154 0.0016 0.0408 1.0000 19.000 1.2903 0.08947 0.08432 0.0010 0.0388 1.0000 19.250 1.2892 0.09281 0.08769 0.0001 0.0370 1.0000