XFOIL Version 6.96 Calculated polar for: Rhode St. Genese 36 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 ------ -------- --------- --------- -------- -------- -------- -13.000 -0.0309 0.09277 0.08860 -0.1004 0.9522 0.0428 -12.750 -0.0272 0.08792 0.08373 -0.1043 0.9475 0.0430 -12.500 -0.0307 0.08403 0.07984 -0.1056 0.9383 0.0431 -12.250 -0.0316 0.08087 0.07669 -0.1061 0.9281 0.0430 -12.000 -0.0383 0.07712 0.07296 -0.1068 0.9163 0.0430 -11.500 -0.0604 0.06873 0.06460 -0.1087 0.8841 0.0429 -11.250 -0.1970 0.04577 0.04127 -0.1234 0.8580 0.0426 -11.000 -0.2626 0.03664 0.03127 -0.1213 0.8440 0.0431 -10.750 -0.2656 0.03342 0.02757 -0.1192 0.8342 0.0436 -10.500 -0.2485 0.03232 0.02635 -0.1180 0.8250 0.0440 -10.250 -0.2312 0.03122 0.02511 -0.1168 0.8159 0.0444 -10.000 -0.2147 0.02994 0.02363 -0.1155 0.8068 0.0449 -9.750 -0.1987 0.02853 0.02196 -0.1142 0.7984 0.0454 -9.500 -0.1820 0.02714 0.02029 -0.1128 0.7894 0.0460 -9.250 -0.1639 0.02579 0.01863 -0.1116 0.7816 0.0466 -9.000 -0.1454 0.02454 0.01709 -0.1102 0.7721 0.0474 -8.750 -0.1250 0.02336 0.01552 -0.1090 0.7644 0.0481 -8.500 -0.1030 0.02259 0.01464 -0.1080 0.7558 0.0488 -8.250 -0.0790 0.02206 0.01405 -0.1073 0.7483 0.0495 -8.000 -0.0553 0.02153 0.01344 -0.1065 0.7400 0.0504 -7.750 -0.0314 0.02095 0.01273 -0.1057 0.7311 0.0514 -7.500 -0.0073 0.02032 0.01194 -0.1048 0.7233 0.0523 -7.250 0.0168 0.01971 0.01115 -0.1040 0.7145 0.0533 -7.000 0.0417 0.01914 0.01044 -0.1032 0.7061 0.0541 -6.750 0.0663 0.01867 0.00996 -0.1025 0.6963 0.0550 -6.500 0.0915 0.01828 0.00951 -0.1018 0.6877 0.0561 -6.250 0.1164 0.01791 0.00907 -0.1011 0.6782 0.0575 -6.000 0.1417 0.01758 0.00859 -0.1004 0.6690 0.0591 -5.750 0.1663 0.01719 0.00814 -0.0996 0.6581 0.0603 -5.500 0.1907 0.01684 0.00777 -0.0988 0.6472 0.0615 -5.250 0.2150 0.01656 0.00742 -0.0979 0.6356 0.0629 -5.000 0.2395 0.01633 0.00712 -0.0971 0.6253 0.0647 -4.750 0.2638 0.01612 0.00682 -0.0962 0.6144 0.0665 -4.500 0.2873 0.01584 0.00656 -0.0953 0.6033 0.0682 -4.250 0.3107 0.01566 0.00632 -0.0943 0.5909 0.0702 -4.000 0.3339 0.01550 0.00612 -0.0933 0.5761 0.0722 -3.750 0.3561 0.01532 0.00590 -0.0921 0.5580 0.0744 -3.500 0.3769 0.01522 0.00571 -0.0907 0.5322 0.0770 -3.250 0.3944 0.01526 0.00554 -0.0887 0.4875 0.0796 -3.000 0.4079 0.01544 0.00545 -0.0860 0.4480 0.0819 -2.500 0.4414 0.01568 0.00545 -0.0819 0.4106 0.0902 -2.250 0.4600 0.01573 0.00551 -0.0802 0.4001 0.0987 -2.000 0.4793 0.01580 0.00567 -0.0787 0.3912 0.1302 -1.750 0.4988 0.01598 0.00577 -0.0771 0.3841 0.1518 -1.500 0.5198 0.01604 0.00585 -0.0759 0.3779 0.1684 -1.250 0.5396 0.01615 0.00593 -0.0744 0.3722 0.1803 -1.000 0.5581 0.01626 0.00603 -0.0727 0.3673 0.1930 -0.750 0.5776 0.01634 0.00614 -0.0713 0.3632 0.2111 -0.500 0.5979 0.01637 0.00626 -0.0700 0.3590 0.2384 -0.250 0.6169 0.01633 0.00641 -0.0685 0.3549 0.3031 0.000 0.6269 0.01565 0.00667 -0.0655 0.3513 0.6005 0.500 0.7633 0.01602 0.00764 -0.0819 0.3418 1.0000 1.000 0.7974 0.01643 0.00794 -0.0781 0.3365 1.0000 1.250 0.8151 0.01666 0.00811 -0.0764 0.3341 1.0000 1.500 0.8333 0.01692 0.00829 -0.0748 0.3316 1.0000 1.750 0.8521 0.01720 0.00850 -0.0733 0.3294 1.0000 2.000 0.8718 0.01751 0.00872 -0.0720 0.3273 1.0000 2.250 0.8929 0.01784 0.00896 -0.0711 0.3252 1.0000 2.500 0.9133 0.01809 0.00920 -0.0699 0.3233 1.0000 2.750 0.9339 0.01835 0.00945 -0.0689 0.3214 1.0000 3.000 0.9541 0.01863 0.00972 -0.0678 0.3191 1.0000 3.250 0.9747 0.01892 0.00999 -0.0668 0.3171 1.0000 3.500 0.9952 0.01923 0.01028 -0.0659 0.3150 1.0000 3.750 1.0161 0.01955 0.01058 -0.0650 0.3133 1.0000 4.000 1.0372 0.01989 0.01088 -0.0642 0.3116 1.0000 4.250 1.0589 0.02024 0.01120 -0.0635 0.3100 1.0000 4.500 1.0813 0.02062 0.01153 -0.0630 0.3083 1.0000 4.750 1.1054 0.02102 0.01188 -0.0628 0.3068 1.0000 5.000 1.1273 0.02138 0.01226 -0.0622 0.3055 1.0000 5.250 1.1479 0.02174 0.01266 -0.0615 0.3042 1.0000 5.500 1.1687 0.02212 0.01308 -0.0608 0.3029 1.0000 5.750 1.1892 0.02251 0.01351 -0.0601 0.3014 1.0000 6.000 1.2092 0.02291 0.01395 -0.0593 0.2997 1.0000 6.250 1.2289 0.02333 0.01439 -0.0586 0.2980 1.0000 6.500 1.2478 0.02374 0.01484 -0.0577 0.2961 1.0000 6.750 1.2655 0.02416 0.01527 -0.0567 0.2940 1.0000 7.000 1.2837 0.02460 0.01570 -0.0558 0.2920 1.0000 7.250 1.3039 0.02505 0.01613 -0.0553 0.2900 1.0000 7.500 1.3255 0.02553 0.01658 -0.0549 0.2878 1.0000 7.750 1.3395 0.02606 0.01721 -0.0536 0.2861 1.0000 8.000 1.3540 0.02661 0.01785 -0.0524 0.2841 1.0000 8.250 1.3698 0.02717 0.01849 -0.0513 0.2823 1.0000 8.500 1.3844 0.02775 0.01915 -0.0502 0.2801 1.0000 8.750 1.4005 0.02833 0.01979 -0.0494 0.2784 1.0000 9.000 1.4159 0.02893 0.02044 -0.0485 0.2766 1.0000 9.250 1.4313 0.02954 0.02109 -0.0476 0.2748 1.0000 9.500 1.4470 0.03013 0.02168 -0.0468 0.2728 1.0000 9.750 1.4640 0.03072 0.02226 -0.0462 0.2705 1.0000 10.000 1.4710 0.03167 0.02336 -0.0446 0.2681 1.0000 10.250 1.4815 0.03257 0.02439 -0.0435 0.2660 1.0000 10.500 1.4926 0.03346 0.02539 -0.0425 0.2640 1.0000 10.750 1.5034 0.03439 0.02640 -0.0415 0.2619 1.0000 11.000 1.5145 0.03532 0.02741 -0.0406 0.2600 1.0000 11.250 1.5255 0.03626 0.02842 -0.0398 0.2581 1.0000 11.500 1.5379 0.03713 0.02933 -0.0391 0.2562 1.0000 11.750 1.5523 0.03793 0.03014 -0.0386 0.2545 1.0000 12.000 1.5550 0.03951 0.03190 -0.0375 0.2520 1.0000 12.500 1.5636 0.04265 0.03533 -0.0357 0.2468 1.0000 12.750 1.5690 0.04420 0.03699 -0.0350 0.2443 1.0000 13.000 1.5747 0.04573 0.03857 -0.0344 0.2416 1.0000 13.250 1.5832 0.04704 0.03990 -0.0340 0.2391 1.0000 13.500 1.5799 0.04958 0.04265 -0.0333 0.2357 1.0000 13.750 1.5775 0.05216 0.04540 -0.0328 0.2323 1.0000 14.000 1.5768 0.05463 0.04799 -0.0326 0.2289 1.0000 14.250 1.5782 0.05691 0.05034 -0.0324 0.2259 1.0000 14.500 1.5752 0.05978 0.05332 -0.0323 0.2224 1.0000 14.750 1.5618 0.06401 0.05776 -0.0324 0.2180 1.0000 15.000 1.5503 0.06813 0.06202 -0.0327 0.2135 1.0000 15.250 1.5423 0.07192 0.06589 -0.0331 0.2095 1.0000 15.500 1.5005 0.08049 0.07474 -0.0343 0.2047 1.0000 15.750 1.4277 0.09424 0.08872 -0.0373 0.1987 1.0000