XFOIL Version 6.96 Calculated polar for: SG6050 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.250 -0.8413 0.09341 0.08977 -0.0434 1.0000 0.0070 -16.000 -0.8696 0.08448 0.08069 -0.0481 1.0000 0.0069 -15.750 -0.8984 0.07603 0.07210 -0.0527 1.0000 0.0069 -15.500 -0.9236 0.06849 0.06443 -0.0569 1.0000 0.0069 -15.250 -0.9459 0.06159 0.05739 -0.0608 1.0000 0.0069 -15.000 -0.9642 0.05529 0.05096 -0.0646 1.0000 0.0069 -14.750 -0.9780 0.04949 0.04503 -0.0684 1.0000 0.0069 -14.500 -0.9866 0.04416 0.03954 -0.0723 1.0000 0.0069 -14.250 -0.9911 0.03945 0.03468 -0.0760 1.0000 0.0070 -14.000 -0.9963 0.03519 0.03027 -0.0792 1.0000 0.0070 -13.750 -1.0003 0.03204 0.02699 -0.0805 1.0000 0.0071 -13.500 -1.0034 0.02980 0.02465 -0.0799 1.0000 0.0072 -13.250 -1.0045 0.02817 0.02292 -0.0782 0.9956 0.0074 -13.000 -0.9909 0.02668 0.02132 -0.0783 0.9801 0.0075 -12.750 -0.9745 0.02544 0.01997 -0.0782 0.9601 0.0078 -12.500 -0.9575 0.02437 0.01878 -0.0777 0.9408 0.0080 -12.250 -0.9421 0.02346 0.01772 -0.0766 0.9225 0.0082 -12.000 -0.9257 0.02264 0.01675 -0.0754 0.9065 0.0085 -11.750 -0.9078 0.02188 0.01585 -0.0744 0.8929 0.0088 -11.500 -0.8882 0.02114 0.01499 -0.0736 0.8814 0.0090 -11.250 -0.8684 0.02035 0.01409 -0.0730 0.8715 0.0095 -11.000 -0.8471 0.01967 0.01329 -0.0724 0.8619 0.0100 -10.750 -0.8246 0.01904 0.01255 -0.0720 0.8534 0.0107 -10.500 -0.8016 0.01844 0.01184 -0.0716 0.8453 0.0115 -10.250 -0.7782 0.01780 0.01114 -0.0714 0.8385 0.0130 -10.000 -0.7543 0.01719 0.01046 -0.0712 0.8316 0.0152 -9.750 -0.7302 0.01660 0.00980 -0.0710 0.8254 0.0190 -9.500 -0.7053 0.01602 0.00921 -0.0709 0.8190 0.0242 -9.250 -0.6799 0.01554 0.00873 -0.0709 0.8130 0.0308 -9.000 -0.6534 0.01518 0.00835 -0.0710 0.8079 0.0369 -8.750 -0.6262 0.01486 0.00801 -0.0711 0.8023 0.0414 -8.500 -0.5988 0.01460 0.00770 -0.0713 0.7969 0.0454 -8.250 -0.5714 0.01434 0.00737 -0.0714 0.7920 0.0482 -8.000 -0.5436 0.01407 0.00709 -0.0717 0.7868 0.0514 -7.750 -0.5154 0.01388 0.00682 -0.0719 0.7817 0.0543 -7.500 -0.4878 0.01360 0.00651 -0.0721 0.7771 0.0577 -7.250 -0.4595 0.01337 0.00626 -0.0724 0.7725 0.0612 -7.000 -0.4308 0.01320 0.00603 -0.0727 0.7677 0.0641 -6.750 -0.4029 0.01291 0.00572 -0.0730 0.7632 0.0681 -6.500 -0.3745 0.01268 0.00545 -0.0733 0.7590 0.0713 -6.250 -0.3457 0.01247 0.00520 -0.0736 0.7545 0.0739 -6.000 -0.3169 0.01227 0.00494 -0.0740 0.7500 0.0764 -5.750 -0.2883 0.01203 0.00468 -0.0743 0.7456 0.0802 -5.500 -0.2594 0.01183 0.00445 -0.0746 0.7417 0.0843 -5.250 -0.2303 0.01164 0.00424 -0.0750 0.7373 0.0893 -5.000 -0.2013 0.01142 0.00403 -0.0754 0.7328 0.0968 -4.750 -0.1724 0.01123 0.00382 -0.0758 0.7286 0.1057 -4.500 -0.1433 0.01102 0.00363 -0.0762 0.7244 0.1186 -4.250 -0.1142 0.01076 0.00344 -0.0767 0.7196 0.1380 -4.000 -0.0854 0.01047 0.00324 -0.0771 0.7146 0.1678 -3.750 -0.0569 0.01011 0.00303 -0.0776 0.7102 0.2170 -3.500 -0.0279 0.00980 0.00291 -0.0781 0.7053 0.2658 -3.250 0.0014 0.00964 0.00284 -0.0786 0.7003 0.2981 -3.000 0.0309 0.00957 0.00279 -0.0790 0.6957 0.3191 -2.750 0.0606 0.00952 0.00274 -0.0794 0.6911 0.3346 -2.500 0.0904 0.00948 0.00271 -0.0799 0.6859 0.3481 -2.250 0.1201 0.00944 0.00266 -0.0803 0.6808 0.3582 -2.000 0.1498 0.00944 0.00262 -0.0808 0.6761 0.3659 -1.750 0.1796 0.00940 0.00260 -0.0812 0.6705 0.3763 -1.500 0.2091 0.00938 0.00260 -0.0817 0.6650 0.3925 -1.250 0.2387 0.00936 0.00258 -0.0821 0.6597 0.4046 -1.000 0.2684 0.00934 0.00256 -0.0825 0.6536 0.4107 -0.750 0.2979 0.00935 0.00252 -0.0829 0.6474 0.4148 -0.500 0.3275 0.00933 0.00250 -0.0834 0.6413 0.4188 -0.250 0.3570 0.00931 0.00248 -0.0838 0.6346 0.4238 0.000 0.3864 0.00933 0.00247 -0.0842 0.6287 0.4288 0.250 0.4160 0.00933 0.00247 -0.0846 0.6220 0.4335 0.500 0.4453 0.00933 0.00248 -0.0850 0.6155 0.4396 0.750 0.4747 0.00934 0.00249 -0.0854 0.6089 0.4459 1.000 0.5040 0.00935 0.00252 -0.0858 0.6018 0.4531 1.250 0.5332 0.00936 0.00255 -0.0862 0.5949 0.4621 1.500 0.5623 0.00937 0.00258 -0.0866 0.5866 0.4724 1.750 0.5913 0.00938 0.00263 -0.0870 0.5786 0.4862 2.000 0.6202 0.00938 0.00269 -0.0874 0.5696 0.5074 2.250 0.6490 0.00936 0.00276 -0.0877 0.5612 0.5387 2.500 0.6775 0.00931 0.00285 -0.0881 0.5524 0.5843 2.750 0.7059 0.00923 0.00295 -0.0884 0.5437 0.6436 3.000 0.7333 0.00915 0.00307 -0.0885 0.5348 0.7131 3.250 0.7586 0.00901 0.00324 -0.0879 0.5259 0.8023 3.500 0.7817 0.00904 0.00339 -0.0867 0.5171 0.8698 3.750 0.8064 0.00910 0.00351 -0.0860 0.5078 0.8993 4.000 0.8307 0.00921 0.00363 -0.0852 0.4985 0.9220 4.250 0.8550 0.00932 0.00375 -0.0844 0.4883 0.9423 4.500 0.8816 0.00945 0.00386 -0.0842 0.4766 0.9632 4.750 0.9104 0.00961 0.00400 -0.0846 0.4641 0.9840 5.000 0.9401 0.00978 0.00413 -0.0853 0.4518 1.0000 5.250 0.9666 0.01001 0.00431 -0.0852 0.4396 1.0000 5.500 0.9932 0.01023 0.00450 -0.0852 0.4277 1.0000 5.750 1.0193 0.01048 0.00472 -0.0851 0.4152 1.0000 6.000 1.0448 0.01075 0.00495 -0.0850 0.4017 1.0000 6.250 1.0700 0.01104 0.00519 -0.0847 0.3885 1.0000 6.500 1.0948 0.01135 0.00546 -0.0844 0.3750 1.0000 6.750 1.1194 0.01165 0.00573 -0.0841 0.3610 1.0000 7.000 1.1431 0.01200 0.00604 -0.0837 0.3460 1.0000 7.250 1.1658 0.01239 0.00637 -0.0830 0.3297 1.0000 7.500 1.1878 0.01281 0.00673 -0.0823 0.3134 1.0000 7.750 1.2092 0.01323 0.00711 -0.0814 0.2974 1.0000 8.000 1.2296 0.01369 0.00752 -0.0804 0.2811 1.0000 8.250 1.2484 0.01420 0.00797 -0.0792 0.2631 1.0000 8.500 1.2643 0.01483 0.00850 -0.0774 0.2410 1.0000 8.750 1.2760 0.01554 0.00910 -0.0750 0.2186 1.0000 9.000 1.2863 0.01630 0.00978 -0.0723 0.1975 1.0000 9.250 1.2963 0.01716 0.01054 -0.0698 0.1781 1.0000 9.500 1.3064 0.01810 0.01139 -0.0675 0.1595 1.0000 9.750 1.3163 0.01910 0.01232 -0.0654 0.1416 1.0000 10.000 1.3262 0.02017 0.01332 -0.0634 0.1256 1.0000 10.250 1.3356 0.02133 0.01442 -0.0615 0.1107 1.0000 10.500 1.3450 0.02253 0.01558 -0.0598 0.0978 1.0000 10.750 1.3543 0.02380 0.01682 -0.0582 0.0861 1.0000 11.000 1.3638 0.02511 0.01810 -0.0567 0.0763 1.0000 11.250 1.3729 0.02648 0.01945 -0.0553 0.0676 1.0000 11.500 1.3814 0.02793 0.02089 -0.0539 0.0601 1.0000 11.750 1.3896 0.02944 0.02241 -0.0526 0.0533 1.0000 12.000 1.3981 0.03096 0.02393 -0.0514 0.0475 1.0000 12.250 1.4052 0.03262 0.02560 -0.0502 0.0422 1.0000 12.500 1.4116 0.03437 0.02737 -0.0490 0.0374 1.0000 12.750 1.4186 0.03610 0.02913 -0.0480 0.0333 1.0000 13.000 1.4241 0.03798 0.03105 -0.0469 0.0300 1.0000 13.250 1.4292 0.03994 0.03305 -0.0459 0.0268 1.0000 13.500 1.4342 0.04196 0.03511 -0.0450 0.0242 1.0000 13.750 1.4378 0.04416 0.03735 -0.0442 0.0218 1.0000 14.000 1.4424 0.04633 0.03958 -0.0435 0.0197 1.0000 14.250 1.4447 0.04878 0.04208 -0.0428 0.0179 1.0000 14.500 1.4483 0.05118 0.04454 -0.0422 0.0162 1.0000 14.750 1.4498 0.05385 0.04727 -0.0418 0.0147 1.0000 15.000 1.4521 0.05647 0.04997 -0.0414 0.0134 1.0000 15.250 1.4529 0.05932 0.05289 -0.0411 0.0124 1.0000 15.500 1.4534 0.06228 0.05592 -0.0409 0.0116 1.0000 15.750 1.4540 0.06529 0.05901 -0.0408 0.0108 1.0000 16.000 1.4533 0.06849 0.06229 -0.0409 0.0103 1.0000 16.250 1.4513 0.07190 0.06578 -0.0410 0.0098 1.0000 16.500 1.4491 0.07542 0.06939 -0.0412 0.0094 1.0000 16.750 1.4473 0.07894 0.07301 -0.0415 0.0091 1.0000 17.000 1.4448 0.08261 0.07677 -0.0420 0.0089 1.0000 17.250 1.4415 0.08641 0.08068 -0.0426 0.0086 1.0000 17.500 1.4373 0.09038 0.08475 -0.0432 0.0084 1.0000 17.750 1.4325 0.09451 0.08897 -0.0440 0.0082 1.0000 18.000 1.4269 0.09882 0.09338 -0.0450 0.0081 1.0000 18.250 1.4207 0.10327 0.09792 -0.0461 0.0079 1.0000 18.500 1.4135 0.10788 0.10264 -0.0474 0.0078 1.0000 18.750 1.4053 0.11275 0.10760 -0.0489 0.0076 1.0000