GOE 16K AIRFOIL (goe16k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 16K AIRFOIL (goe16k-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.87 at α=2.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe16k-il-1000000-n5.txt Download as CSV file: xf-goe16k-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 16K AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.6958 0.07375 0.07025 -0.1756 0.9477 0.0154
-19.500 -0.7271 0.06649 0.06285 -0.1797 0.9471 0.0153
-19.250 -0.7569 0.05950 0.05571 -0.1836 0.9466 0.0154
-19.000 -0.7774 0.05357 0.04966 -0.1873 0.9461 0.0156
-18.750 -0.8235 0.04814 0.04410 -0.1853 0.9398 0.0161
-18.500 -0.8339 0.04399 0.03984 -0.1874 0.9379 0.0163
-18.250 -0.8398 0.04030 0.03602 -0.1893 0.9363 0.0162
-18.000 -0.8467 0.03679 0.03240 -0.1908 0.9350 0.0169
-17.750 -0.8475 0.03417 0.02968 -0.1914 0.9339 0.0170
-17.500 -0.8647 0.03229 0.02770 -0.1876 0.9272 0.0170
-17.250 -0.8655 0.03048 0.02580 -0.1866 0.9245 0.0176
-17.000 -0.8604 0.02885 0.02409 -0.1860 0.9228 0.0185
-16.750 -0.8525 0.02737 0.02253 -0.1856 0.9214 0.0185
-16.500 -0.8474 0.02596 0.02105 -0.1844 0.9193 0.0194
-16.250 -0.8477 0.02484 0.01987 -0.1817 0.9144 0.0205
-16.000 -0.8369 0.02379 0.01874 -0.1807 0.9117 0.0210
-15.750 -0.8223 0.02277 0.01766 -0.1804 0.9097 0.0223
-15.500 -0.8042 0.02180 0.01663 -0.1806 0.9081 0.0235
-15.250 -0.7838 0.02096 0.01572 -0.1810 0.9064 0.0244
-15.000 -0.7737 0.02033 0.01503 -0.1790 0.9017 0.0253
-14.750 -0.7578 0.01966 0.01433 -0.1781 0.8979 0.0274
-14.500 -0.7367 0.01907 0.01370 -0.1782 0.8949 0.0290
-14.250 -0.7131 0.01852 0.01307 -0.1787 0.8923 0.0303
-14.000 -0.6974 0.01808 0.01260 -0.1774 0.8883 0.0317
-13.750 -0.6811 0.01770 0.01219 -0.1760 0.8836 0.0332
-13.500 -0.6599 0.01734 0.01177 -0.1757 0.8800 0.0345
-13.250 -0.6359 0.01694 0.01129 -0.1759 0.8769 0.0353
-13.000 -0.6213 0.01658 0.01086 -0.1741 0.8729 0.0356
-12.750 -0.6068 0.01633 0.01059 -0.1720 0.8688 0.0371
-12.500 -0.5912 0.01599 0.01019 -0.1704 0.8650 0.0372
-12.250 -0.5701 0.01573 0.00990 -0.1697 0.8620 0.0384
-12.000 -0.5482 0.01547 0.00959 -0.1692 0.8592 0.0395
-11.750 -0.5346 0.01533 0.00942 -0.1667 0.8562 0.0407
-11.500 -0.5207 0.01515 0.00919 -0.1644 0.8530 0.0413
-11.250 -0.5039 0.01497 0.00897 -0.1626 0.8502 0.0419
-11.000 -0.4855 0.01477 0.00871 -0.1612 0.8476 0.0423
-10.750 -0.4675 0.01449 0.00837 -0.1598 0.8451 0.0424
-10.250 -0.4342 0.01401 0.00786 -0.1561 0.8408 0.0447
-10.000 -0.4196 0.01386 0.00769 -0.1538 0.8387 0.0456
-9.750 -0.4044 0.01366 0.00745 -0.1515 0.8366 0.0457
-9.500 -0.3863 0.01353 0.00730 -0.1499 0.8347 0.0469
-9.250 -0.3681 0.01335 0.00708 -0.1482 0.8327 0.0474
-9.000 -0.3481 0.01320 0.00690 -0.1470 0.8311 0.0480
-8.750 -0.3276 0.01303 0.00667 -0.1458 0.8293 0.0483
-8.500 -0.3053 0.01287 0.00647 -0.1450 0.8276 0.0489
-8.000 -0.2640 0.01257 0.00611 -0.1427 0.8247 0.0497
-7.750 -0.2482 0.01242 0.00594 -0.1404 0.8232 0.0496
-7.500 -0.2316 0.01220 0.00571 -0.1383 0.8219 0.0517
-7.250 -0.2134 0.01203 0.00553 -0.1366 0.8205 0.0522
-7.000 -0.1942 0.01190 0.00539 -0.1351 0.8192 0.0531
-6.750 -0.1741 0.01177 0.00524 -0.1337 0.8178 0.0534
-6.500 -0.1529 0.01163 0.00510 -0.1326 0.8166 0.0545
-6.250 -0.1310 0.01152 0.00497 -0.1316 0.8154 0.0554
-6.000 -0.1082 0.01140 0.00483 -0.1308 0.8143 0.0558
-5.750 -0.0846 0.01129 0.00469 -0.1302 0.8131 0.0570
-5.500 -0.0597 0.01118 0.00456 -0.1299 0.8121 0.0573
-5.250 -0.0336 0.01109 0.00446 -0.1298 0.8111 0.0580
-5.000 -0.0058 0.01095 0.00430 -0.1302 0.8100 0.0588
-4.750 0.0227 0.01083 0.00418 -0.1307 0.8091 0.0607
-4.500 0.0408 0.01074 0.00411 -0.1288 0.8083 0.0632
-4.250 0.0589 0.01067 0.00405 -0.1269 0.8073 0.0650
-4.000 0.0776 0.01062 0.00401 -0.1251 0.8061 0.0653
-3.750 0.0970 0.01056 0.00396 -0.1235 0.8049 0.0674
-3.500 0.1178 0.01046 0.00391 -0.1223 0.8038 0.0744
-3.250 0.1390 0.01029 0.00384 -0.1211 0.8027 0.0951
-3.000 0.1601 0.01022 0.00380 -0.1199 0.8017 0.1057
-2.750 0.1816 0.00999 0.00375 -0.1189 0.8007 0.1497
-2.500 0.2037 0.00985 0.00373 -0.1180 0.7997 0.1781
-2.250 0.2265 0.00977 0.00371 -0.1172 0.7987 0.1937
-2.000 0.2503 0.00969 0.00369 -0.1166 0.7976 0.2113
-1.750 0.2757 0.00958 0.00366 -0.1164 0.7964 0.2333
-1.500 0.3057 0.00943 0.00359 -0.1173 0.7941 0.2617
-1.250 0.3359 0.00933 0.00356 -0.1182 0.7925 0.2849
-1.000 0.3390 0.00938 0.00367 -0.1127 0.7902 0.2958
-0.750 0.3528 0.00936 0.00373 -0.1099 0.7882 0.3161
-0.500 0.3707 0.00936 0.00377 -0.1079 0.7864 0.3277
-0.250 0.3873 0.00930 0.00382 -0.1056 0.7840 0.3586
0.000 0.4076 0.00928 0.00385 -0.1042 0.7825 0.3724
0.250 0.4292 0.00923 0.00383 -0.1031 0.7795 0.3885
0.500 0.4559 0.00917 0.00382 -0.1031 0.7780 0.4058
0.750 0.4799 0.00904 0.00384 -0.1026 0.7760 0.4521
1.000 0.4913 0.00891 0.00396 -0.0993 0.7749 0.5219
1.250 0.5017 0.00900 0.00410 -0.0956 0.7724 0.5320
1.750 0.6435 0.00941 0.00583 -0.1159 0.7709 0.9029
2.000 0.6558 0.00968 0.00611 -0.1125 0.7671 0.9136
2.250 0.6782 0.00976 0.00620 -0.1116 0.7663 0.9171
2.500 0.7060 0.00999 0.00642 -0.1117 0.7630 0.9233
2.750 0.7165 0.01011 0.00654 -0.1080 0.7593 0.9306
3.000 0.7253 0.01055 0.00701 -0.1040 0.7514 0.9330
3.250 0.7516 0.01070 0.00718 -0.1040 0.7504 0.9351
3.500 0.7618 0.01091 0.00737 -0.1003 0.7431 0.9399
3.750 0.7653 0.01140 0.00784 -0.0951 0.7299 0.9442
4.000 0.7870 0.01175 0.00822 -0.0941 0.7215 0.9460
4.250 0.7604 0.01285 0.00909 -0.0826 0.6703 0.9513
4.500 0.7551 0.01356 0.00971 -0.0758 0.6491 0.9548
4.750 0.7643 0.01458 0.01060 -0.0726 0.6194 0.9565
5.000 0.7615 0.01584 0.01171 -0.0670 0.5831 0.9588
5.250 0.7215 0.01784 0.01339 -0.0540 0.5108 0.9630
5.500 0.7188 0.01919 0.01456 -0.0488 0.4675 0.9655
5.750 0.7208 0.02038 0.01553 -0.0448 0.4235 0.9662
6.000 0.7364 0.02107 0.01614 -0.0433 0.4046 0.9669
6.250 0.7576 0.02182 0.01681 -0.0430 0.3837 0.9683
6.500 0.7752 0.02241 0.01734 -0.0418 0.3667 0.9694
6.750 0.7935 0.02309 0.01795 -0.0408 0.3489 0.9716
7.000 0.7833 0.02419 0.01893 -0.0336 0.3217 0.9749
7.250 0.8146 0.02450 0.01925 -0.0354 0.3157 0.9754
7.500 0.8350 0.02503 0.01970 -0.0350 0.2968 0.9758
7.750 0.8469 0.02579 0.02030 -0.0330 0.2644 0.9762
8.000 0.8550 0.02662 0.02098 -0.0303 0.2334 0.9765
8.250 0.8660 0.02755 0.02172 -0.0284 0.1969 0.9770
8.500 0.8830 0.02808 0.02220 -0.0272 0.1848 0.9774
8.750 0.8991 0.02869 0.02274 -0.0260 0.1684 0.9780
9.000 0.9140 0.02936 0.02332 -0.0246 0.1502 0.9785
9.250 0.9323 0.02980 0.02378 -0.0236 0.1480 0.9790
9.500 0.9463 0.03043 0.02435 -0.0220 0.1355 0.9795
9.750 0.9596 0.03109 0.02493 -0.0203 0.1216 0.9800
10.000 0.9736 0.03173 0.02551 -0.0186 0.1105 0.9804
10.250 0.9869 0.03237 0.02610 -0.0170 0.0990 0.9810
10.500 1.0016 0.03295 0.02668 -0.0154 0.0955 0.9815
10.750 1.0150 0.03365 0.02737 -0.0137 0.0903 0.9824
11.250 1.0373 0.03525 0.02896 -0.0091 0.0815 0.9849
11.500 1.0472 0.03615 0.02971 -0.0073 0.0644 0.9850
11.750 1.0682 0.03644 0.03011 -0.0069 0.0711 0.9851
12.000 1.0803 0.03723 0.03086 -0.0054 0.0624 0.9853
12.250 1.0932 0.03798 0.03156 -0.0041 0.0562 0.9854
12.500 1.1100 0.03851 0.03214 -0.0032 0.0562 0.9855
12.750 1.1249 0.03918 0.03281 -0.0021 0.0523 0.9856
13.000 1.1379 0.04009 0.03367 -0.0010 0.0442 0.9859
13.250 1.1572 0.04061 0.03430 -0.0007 0.0491 0.9861
13.500 1.1682 0.04153 0.03517 0.0008 0.0423 0.9862
13.750 1.1796 0.04238 0.03601 0.0023 0.0374 0.9863
14.000 1.1878 0.04345 0.03705 0.0041 0.0317 0.9863
14.250 1.1999 0.04428 0.03792 0.0055 0.0312 0.9864
14.500 1.2085 0.04533 0.03896 0.0072 0.0274 0.9864
14.750 1.2188 0.04629 0.03994 0.0087 0.0258 0.9865
15.000 1.2266 0.04742 0.04109 0.0105 0.0239 0.9865
15.250 1.2361 0.04845 0.04215 0.0120 0.0222 0.9865
15.500 1.2473 0.04935 0.04309 0.0133 0.0225 0.9865
15.750 1.2543 0.05059 0.04437 0.0149 0.0211 0.9866
16.000 1.2612 0.05183 0.04563 0.0166 0.0193 0.9866
16.250 1.2692 0.05299 0.04682 0.0180 0.0182 0.9866
16.500 1.2778 0.05415 0.04804 0.0194 0.0187 0.9866
16.750 1.2836 0.05555 0.04946 0.0209 0.0172 0.9866
17.000 1.2885 0.05704 0.05099 0.0224 0.0166 0.9866
17.250 1.2968 0.05829 0.05229 0.0236 0.0158 0.9866
17.500 1.3024 0.05979 0.05384 0.0249 0.0152 0.9867
17.750 1.3086 0.06146 0.05555 0.0258 0.0145 0.9868
18.000 1.3147 0.06317 0.05729 0.0265 0.0135 0.9870
18.250 1.3203 0.06480 0.05897 0.0275 0.0131 0.9871
18.500 1.3245 0.06646 0.06070 0.0286 0.0132 0.9871
18.750 1.3268 0.06838 0.06267 0.0298 0.0120 0.9871
19.000 1.3295 0.07026 0.06461 0.0308 0.0122 0.9871
19.250 1.3318 0.07221 0.06664 0.0318 0.0126 0.9871
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