XFOIL Version 6.96 Calculated polar for: GOE 575 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 = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -15.000 -1.0378 0.04310 0.03922 -0.0953 0.9890 0.0269 -14.750 -1.0379 0.04115 0.03718 -0.0946 0.9878 0.0271 -14.500 -1.0285 0.04010 0.03607 -0.0938 0.9869 0.0274 -14.250 -1.0225 0.03869 0.03454 -0.0928 0.9859 0.0276 -14.000 -1.0265 0.03724 0.03301 -0.0890 0.9828 0.0278 -13.750 -1.0194 0.03646 0.03215 -0.0865 0.9810 0.0281 -13.500 -1.0165 0.03524 0.03081 -0.0837 0.9793 0.0283 -13.250 -1.0064 0.03447 0.02993 -0.0816 0.9781 0.0288 -13.000 -0.9975 0.03347 0.02879 -0.0794 0.9771 0.0291 -12.750 -0.9995 0.03256 0.02775 -0.0744 0.9737 0.0295 -12.500 -0.9955 0.03160 0.02664 -0.0708 0.9712 0.0299 -12.250 -0.9873 0.03071 0.02555 -0.0677 0.9695 0.0304 -12.000 -0.9777 0.02972 0.02438 -0.0650 0.9682 0.0307 -11.750 -0.9719 0.02912 0.02372 -0.0610 0.9659 0.0309 -11.500 -0.9663 0.02874 0.02331 -0.0567 0.9628 0.0312 -11.250 -0.9493 0.02837 0.02291 -0.0548 0.9609 0.0315 -11.000 -0.9289 0.02825 0.02277 -0.0535 0.9596 0.0321 -10.750 -0.9099 0.02772 0.02216 -0.0520 0.9586 0.0324 -10.500 -0.8899 0.02715 0.02149 -0.0507 0.9578 0.0329 -10.250 -0.8881 0.02659 0.02084 -0.0455 0.9538 0.0332 -10.000 -0.8716 0.02604 0.02018 -0.0434 0.9514 0.0337 -9.750 -0.8490 0.02535 0.01936 -0.0425 0.9495 0.0343 -9.500 -0.8238 0.02470 0.01854 -0.0421 0.9482 0.0348 -9.250 -0.7978 0.02392 0.01763 -0.0419 0.9473 0.0352 -9.000 -0.7937 0.02344 0.01713 -0.0369 0.9420 0.0355 -8.750 -0.7728 0.02298 0.01665 -0.0355 0.9399 0.0360 -8.500 -0.7479 0.02246 0.01607 -0.0350 0.9383 0.0363 -8.250 -0.7206 0.02194 0.01551 -0.0348 0.9370 0.0367 -8.000 -0.6926 0.02141 0.01492 -0.0349 0.9360 0.0371 -7.750 -0.6851 0.02105 0.01450 -0.0304 0.9298 0.0376 -7.500 -0.6599 0.02057 0.01395 -0.0298 0.9273 0.0382 -7.250 -0.6321 0.02007 0.01338 -0.0297 0.9256 0.0387 -7.000 -0.6032 0.01953 0.01277 -0.0299 0.9244 0.0391 -6.750 -0.5722 0.01908 0.01223 -0.0304 0.9234 0.0398 -6.500 -0.5643 0.01876 0.01187 -0.0260 0.9165 0.0399 -6.250 -0.5374 0.01818 0.01126 -0.0257 0.9141 0.0404 -6.000 -0.5076 0.01763 0.01071 -0.0260 0.9122 0.0409 -5.750 -0.4765 0.01719 0.01026 -0.0266 0.9107 0.0416 -5.500 -0.4445 0.01674 0.00980 -0.0273 0.9095 0.0423 -5.250 -0.4335 0.01652 0.00956 -0.0235 0.9015 0.0429 -5.000 -0.4042 0.01608 0.00910 -0.0236 0.8984 0.0432 -4.750 -0.3729 0.01563 0.00862 -0.0241 0.8961 0.0441 -4.500 -0.3394 0.01516 0.00812 -0.0251 0.8939 0.0447 -4.250 -0.3264 0.01491 0.00784 -0.0216 0.8820 0.0450 -4.000 -0.2918 0.01444 0.00734 -0.0227 0.8776 0.0456 -3.750 -0.2730 0.01411 0.00702 -0.0206 0.8654 0.0461 -3.500 -0.2356 0.01356 0.00648 -0.0225 0.8599 0.0473 -3.250 -0.2061 0.01322 0.00614 -0.0226 0.8470 0.0484 -3.000 -0.1623 0.01272 0.00562 -0.0259 0.8353 0.0493 -2.750 -0.1002 0.01209 0.00492 -0.0331 0.8146 0.0506 -2.500 -0.0281 0.01152 0.00421 -0.0428 0.7796 0.0524 -2.250 0.0180 0.01130 0.00380 -0.0468 0.7417 0.0545 -2.000 0.0449 0.01131 0.00364 -0.0464 0.7106 0.0556 -1.750 0.0683 0.01132 0.00354 -0.0453 0.6881 0.0573 -1.500 0.0911 0.01133 0.00347 -0.0441 0.6702 0.0588 -1.250 0.1143 0.01131 0.00339 -0.0430 0.6540 0.0613 -1.000 0.1372 0.01126 0.00332 -0.0418 0.6375 0.0664 -0.750 0.1611 0.01114 0.00330 -0.0409 0.6212 0.1010 -0.500 0.1828 0.01115 0.00329 -0.0395 0.6047 0.1161 -0.250 0.2040 0.01118 0.00330 -0.0380 0.5859 0.1286 0.000 0.2251 0.01124 0.00331 -0.0364 0.5687 0.1365 0.250 0.2468 0.01128 0.00333 -0.0350 0.5520 0.1485 0.500 0.2676 0.01136 0.00335 -0.0334 0.5318 0.1558 0.750 0.2887 0.01144 0.00338 -0.0320 0.5121 0.1684 1.250 0.3315 0.01160 0.00348 -0.0291 0.4726 0.1955 1.500 0.3538 0.01168 0.00353 -0.0279 0.4573 0.2066 1.750 0.3765 0.01175 0.00358 -0.0269 0.4419 0.2245 2.000 0.3999 0.01178 0.00365 -0.0260 0.4251 0.2534 2.250 0.4286 0.01156 0.00377 -0.0265 0.4088 0.3899 2.750 0.6926 0.01326 0.00682 -0.0734 0.3569 0.9811 3.250 0.7776 0.01352 0.00693 -0.0801 0.3349 0.9891 3.500 0.8427 0.01340 0.00674 -0.0885 0.3239 0.9973 3.750 0.8814 0.01337 0.00663 -0.0911 0.3114 1.0000 4.000 0.9015 0.01354 0.00675 -0.0895 0.3027 1.0000 4.250 0.9219 0.01369 0.00687 -0.0880 0.2939 1.0000 4.500 0.9421 0.01383 0.00700 -0.0864 0.2879 1.0000 4.750 0.9619 0.01401 0.00713 -0.0848 0.2792 1.0000 5.000 0.9814 0.01420 0.00728 -0.0831 0.2692 1.0000 5.250 1.0014 0.01437 0.00744 -0.0815 0.2632 1.0000 5.500 1.0209 0.01456 0.00760 -0.0799 0.2536 1.0000 5.750 1.0396 0.01480 0.00778 -0.0781 0.2398 1.0000 6.000 1.0582 0.01504 0.00798 -0.0763 0.2294 1.0000 6.250 1.0762 0.01532 0.00819 -0.0744 0.2160 1.0000 6.750 1.1118 0.01590 0.00868 -0.0706 0.1936 1.0000 7.000 1.1286 0.01623 0.00895 -0.0685 0.1841 1.0000 7.250 1.1456 0.01653 0.00924 -0.0665 0.1769 1.0000 7.500 1.1622 0.01686 0.00954 -0.0644 0.1705 1.0000 7.750 1.1791 0.01717 0.00984 -0.0623 0.1640 1.0000 8.000 1.1957 0.01749 0.01015 -0.0603 0.1591 1.0000 8.250 1.2123 0.01781 0.01048 -0.0582 0.1543 1.0000 8.500 1.2290 0.01812 0.01080 -0.0562 0.1495 1.0000 8.750 1.2443 0.01849 0.01118 -0.0540 0.1442 1.0000 9.000 1.2599 0.01885 0.01155 -0.0518 0.1403 1.0000 9.250 1.2759 0.01918 0.01191 -0.0497 0.1359 1.0000 9.500 1.2909 0.01958 0.01231 -0.0475 0.1303 1.0000 9.750 1.3052 0.02001 0.01274 -0.0452 0.1237 1.0000 10.000 1.3181 0.02049 0.01321 -0.0428 0.1151 1.0000 10.250 1.3306 0.02101 0.01372 -0.0403 0.1054 1.0000 10.500 1.3409 0.02167 0.01431 -0.0374 0.0940 1.0000 10.750 1.3498 0.02238 0.01498 -0.0345 0.0848 1.0000 11.000 1.3589 0.02310 0.01569 -0.0316 0.0781 1.0000 11.250 1.3688 0.02378 0.01639 -0.0289 0.0744 1.0000 11.500 1.3772 0.02455 0.01718 -0.0260 0.0710 1.0000 11.750 1.3864 0.02529 0.01795 -0.0234 0.0682 1.0000 12.000 1.3960 0.02601 0.01873 -0.0209 0.0671 1.0000 12.250 1.4035 0.02689 0.01963 -0.0181 0.0645 1.0000 12.500 1.4100 0.02785 0.02063 -0.0154 0.0626 1.0000 12.750 1.4154 0.02889 0.02173 -0.0126 0.0609 1.0000 13.000 1.4242 0.02977 0.02267 -0.0104 0.0597 1.0000 13.250 1.4314 0.03076 0.02373 -0.0081 0.0591 1.0000 13.500 1.4373 0.03189 0.02493 -0.0057 0.0581 1.0000 13.750 1.4431 0.03308 0.02618 -0.0035 0.0571 1.0000 14.000 1.4473 0.03442 0.02760 -0.0013 0.0563 1.0000 14.250 1.4514 0.03583 0.02909 0.0007 0.0562 1.0000 14.500 1.4528 0.03752 0.03084 0.0027 0.0549 1.0000 14.750 1.4511 0.03959 0.03296 0.0047 0.0533 1.0000 15.000 1.4514 0.04158 0.03504 0.0063 0.0528 1.0000 15.250 1.4548 0.04340 0.03695 0.0075 0.0521 1.0000 15.500 1.4565 0.04544 0.03910 0.0086 0.0519 1.0000 15.750 1.4574 0.04763 0.04138 0.0096 0.0515 1.0000 16.000 1.4597 0.04974 0.04359 0.0104 0.0505 1.0000 16.250 1.4582 0.05230 0.04625 0.0110 0.0500 1.0000 16.500 1.4563 0.05500 0.04905 0.0115 0.0499 1.0000 16.750 1.4527 0.05798 0.05211 0.0119 0.0485 1.0000 17.000 1.4478 0.06119 0.05541 0.0120 0.0480 1.0000 17.250 1.4425 0.06452 0.05883 0.0120 0.0472 1.0000 17.500 1.4335 0.06837 0.06277 0.0117 0.0464 1.0000 17.750 1.4272 0.07200 0.06651 0.0114 0.0465 1.0000 18.000 1.4174 0.07614 0.07073 0.0107 0.0453 1.0000 18.250 1.4093 0.08011 0.07481 0.0101 0.0451 1.0000 18.500 1.4037 0.08381 0.07862 0.0094 0.0445 1.0000 18.750 1.3975 0.08762 0.08255 0.0086 0.0440 1.0000 19.000 1.3917 0.09144 0.08646 0.0078 0.0427 1.0000 19.250 1.3826 0.09572 0.09086 0.0067 0.0429 1.0000