GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 410 AIRFOIL (goe410-il) Reynolds number: 200,000 Max Cl/Cd: 46.4 at α=6.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe410-il-200000.txt Download as CSV file: xf-goe410-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 410 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7072 0.20454 0.20025 0.0462 1.0000 0.0814
-18.000 -1.1269 0.09694 0.09190 -0.0180 1.0000 0.0696
-17.750 -1.1829 0.08471 0.07929 -0.0257 1.0000 0.0699
-17.500 -1.1555 0.08542 0.08019 -0.0242 1.0000 0.0716
-17.250 -1.1529 0.08251 0.07726 -0.0255 1.0000 0.0728
-17.000 -1.1709 0.07672 0.07132 -0.0287 1.0000 0.0740
-16.750 -1.1928 0.07075 0.06514 -0.0318 1.0000 0.0751
-16.500 -1.2151 0.06512 0.05927 -0.0346 1.0000 0.0762
-16.250 -1.2387 0.05979 0.05365 -0.0369 1.0000 0.0773
-16.000 -1.2399 0.05685 0.05064 -0.0376 1.0000 0.0790
-15.750 -1.2253 0.05583 0.04973 -0.0375 1.0000 0.0809
-15.500 -1.2265 0.05330 0.04712 -0.0381 1.0000 0.0827
-15.250 -1.2364 0.05004 0.04367 -0.0388 1.0000 0.0844
-15.000 -1.2503 0.04677 0.04013 -0.0391 1.0000 0.0861
-14.750 -1.2410 0.04505 0.03844 -0.0388 1.0000 0.0883
-14.500 -1.2305 0.04391 0.03736 -0.0385 1.0000 0.0904
-14.250 -1.2301 0.04217 0.03553 -0.0380 1.0000 0.0926
-14.000 -1.2358 0.04015 0.03330 -0.0371 1.0000 0.0946
-13.750 -1.2403 0.03827 0.03121 -0.0357 1.0000 0.0966
-13.500 -1.2217 0.03744 0.03052 -0.0352 1.0000 0.0990
-13.250 -1.2138 0.03651 0.02958 -0.0339 1.0000 0.1012
-13.000 -1.2117 0.03541 0.02835 -0.0320 1.0000 0.1035
-12.750 -1.2130 0.03436 0.02710 -0.0292 1.0000 0.1056
-12.500 -1.2022 0.03317 0.02586 -0.0276 1.0000 0.1080
-12.250 -1.1857 0.03253 0.02528 -0.0265 1.0000 0.1103
-12.000 -1.1727 0.03187 0.02459 -0.0249 1.0000 0.1128
-11.750 -1.1611 0.03110 0.02369 -0.0232 1.0000 0.1154
-11.500 -1.1499 0.03038 0.02276 -0.0214 1.0000 0.1176
-11.250 -1.1282 0.02919 0.02161 -0.0210 1.0000 0.1203
-11.000 -1.1081 0.02852 0.02098 -0.0201 1.0000 0.1228
-10.750 -1.0897 0.02787 0.02028 -0.0191 1.0000 0.1255
-10.500 -1.0720 0.02721 0.01950 -0.0179 1.0000 0.1283
-10.250 -1.0548 0.02668 0.01879 -0.0165 1.0000 0.1305
-10.000 -1.0307 0.02546 0.01768 -0.0163 1.0000 0.1338
-9.750 -1.0095 0.02487 0.01712 -0.0156 1.0000 0.1370
-9.500 -0.9894 0.02433 0.01652 -0.0146 1.0000 0.1406
-9.250 -0.9692 0.02383 0.01588 -0.0135 1.0000 0.1435
-9.000 -0.9457 0.02273 0.01481 -0.0130 1.0000 0.1465
-8.750 -0.9226 0.02194 0.01409 -0.0124 1.0000 0.1496
-8.500 -0.9001 0.02128 0.01344 -0.0117 1.0000 0.1528
-8.250 -0.8779 0.02067 0.01279 -0.0108 1.0000 0.1560
-8.000 -0.8562 0.02021 0.01221 -0.0098 1.0000 0.1590
-7.750 -0.8342 0.01916 0.01135 -0.0090 1.0000 0.1635
-7.500 -0.8133 0.01854 0.01078 -0.0080 1.0000 0.1678
-7.250 -0.7925 0.01801 0.01024 -0.0068 1.0000 0.1723
-7.000 -0.7736 0.01731 0.00962 -0.0054 1.0000 0.1773
-6.750 -0.7566 0.01669 0.00911 -0.0038 1.0000 0.1831
-6.500 -0.7402 0.01627 0.00870 -0.0020 1.0000 0.1895
-6.250 -0.7270 0.01567 0.00827 0.0000 0.9984 0.1969
-6.000 -0.6821 0.01494 0.00768 -0.0039 0.9835 0.2114
-5.750 -0.6383 0.01420 0.00714 -0.0075 0.9679 0.2350
-5.500 -0.5981 0.01345 0.00670 -0.0104 0.9477 0.2807
-5.250 -0.5624 0.01299 0.00647 -0.0120 0.9224 0.3349
-5.000 -0.5316 0.01285 0.00639 -0.0122 0.8947 0.3690
-4.750 -0.5057 0.01286 0.00632 -0.0113 0.8663 0.3916
-4.500 -0.4814 0.01292 0.00629 -0.0100 0.8408 0.4082
-4.250 -0.4571 0.01298 0.00628 -0.0088 0.8158 0.4217
-4.000 -0.4322 0.01305 0.00623 -0.0078 0.7929 0.4345
-3.750 -0.4069 0.01314 0.00621 -0.0069 0.7718 0.4462
-3.500 -0.3810 0.01318 0.00618 -0.0061 0.7525 0.4563
-3.250 -0.3549 0.01325 0.00612 -0.0054 0.7347 0.4673
-3.000 -0.3284 0.01327 0.00612 -0.0047 0.7186 0.4768
-2.750 -0.3021 0.01336 0.00605 -0.0041 0.7044 0.4883
-2.500 -0.2750 0.01334 0.00608 -0.0035 0.6898 0.4978
-2.250 -0.2480 0.01339 0.00601 -0.0031 0.6771 0.5079
-2.000 -0.2207 0.01334 0.00595 -0.0026 0.6660 0.5155
-1.750 -0.1932 0.01334 0.00591 -0.0023 0.6538 0.5248
-1.500 -0.1657 0.01331 0.00584 -0.0019 0.6443 0.5326
-1.250 -0.1380 0.01330 0.00584 -0.0017 0.6338 0.5416
-1.000 -0.1104 0.01331 0.00576 -0.0013 0.6248 0.5500
-0.750 -0.0827 0.01326 0.00577 -0.0010 0.6140 0.5581
-0.500 -0.0552 0.01330 0.00569 -0.0007 0.6047 0.5673
-0.250 -0.0275 0.01323 0.00571 -0.0004 0.5943 0.5753
0.000 0.0000 0.01330 0.00567 0.0000 0.5856 0.5856
0.250 0.0276 0.01323 0.00571 0.0003 0.5753 0.5943
0.500 0.0552 0.01330 0.00569 0.0007 0.5673 0.6047
0.750 0.0827 0.01326 0.00577 0.0010 0.5581 0.6140
1.000 0.1104 0.01331 0.00576 0.0013 0.5500 0.6249
1.250 0.1380 0.01330 0.00584 0.0017 0.5415 0.6338
1.500 0.1657 0.01331 0.00584 0.0019 0.5326 0.6443
1.750 0.1932 0.01334 0.00591 0.0023 0.5248 0.6539
2.000 0.2207 0.01334 0.00595 0.0026 0.5155 0.6660
2.250 0.2480 0.01339 0.00601 0.0031 0.5079 0.6771
2.500 0.2751 0.01334 0.00608 0.0035 0.4978 0.6898
2.750 0.3021 0.01336 0.00605 0.0041 0.4884 0.7044
3.000 0.3284 0.01327 0.00612 0.0047 0.4768 0.7187
3.250 0.3549 0.01325 0.00612 0.0054 0.4673 0.7347
3.500 0.3810 0.01318 0.00618 0.0061 0.4563 0.7525
3.750 0.4069 0.01314 0.00621 0.0069 0.4462 0.7718
4.000 0.4322 0.01305 0.00623 0.0078 0.4344 0.7929
4.250 0.4571 0.01298 0.00628 0.0088 0.4217 0.8159
4.500 0.4814 0.01292 0.00629 0.0100 0.4082 0.8408
4.750 0.5057 0.01286 0.00632 0.0113 0.3916 0.8663
5.000 0.5316 0.01285 0.00639 0.0122 0.3690 0.8947
5.250 0.5624 0.01299 0.00647 0.0120 0.3350 0.9224
5.500 0.5982 0.01345 0.00670 0.0104 0.2808 0.9477
5.750 0.6384 0.01420 0.00714 0.0075 0.2350 0.9679
6.000 0.6822 0.01494 0.00768 0.0039 0.2114 0.9836
6.250 0.7271 0.01567 0.00827 0.0000 0.1970 0.9984
6.500 0.7402 0.01626 0.00870 0.0020 0.1895 1.0000
6.750 0.7566 0.01669 0.00911 0.0038 0.1831 1.0000
7.000 0.7736 0.01730 0.00962 0.0054 0.1773 1.0000
7.250 0.7925 0.01800 0.01024 0.0068 0.1723 1.0000
7.500 0.8133 0.01854 0.01078 0.0080 0.1678 1.0000
7.750 0.8343 0.01916 0.01135 0.0090 0.1635 1.0000
8.000 0.8562 0.02020 0.01221 0.0098 0.1590 1.0000
8.250 0.8780 0.02067 0.01279 0.0108 0.1560 1.0000
8.500 0.9001 0.02128 0.01344 0.0117 0.1527 1.0000
8.750 0.9226 0.02194 0.01409 0.0124 0.1496 1.0000
9.000 0.9457 0.02273 0.01481 0.0130 0.1465 1.0000
9.250 0.9692 0.02382 0.01588 0.0135 0.1435 1.0000
9.500 0.9894 0.02432 0.01651 0.0146 0.1406 1.0000
9.750 1.0095 0.02486 0.01711 0.0156 0.1370 1.0000
10.000 1.0307 0.02546 0.01768 0.0163 0.1337 1.0000
10.250 1.0550 0.02669 0.01880 0.0165 0.1305 1.0000
10.500 1.0721 0.02721 0.01950 0.0179 0.1282 1.0000
10.750 1.0898 0.02787 0.02028 0.0191 0.1255 1.0000
11.000 1.1082 0.02852 0.02098 0.0201 0.1228 1.0000
11.250 1.1283 0.02917 0.02160 0.0209 0.1202 1.0000
11.500 1.1501 0.03038 0.02275 0.0213 0.1176 1.0000
11.750 1.1612 0.03108 0.02367 0.0232 0.1154 1.0000
12.000 1.1729 0.03187 0.02459 0.0249 0.1128 1.0000
12.250 1.1860 0.03252 0.02528 0.0264 0.1103 1.0000
12.500 1.2025 0.03317 0.02585 0.0276 0.1080 1.0000
12.750 1.2132 0.03435 0.02710 0.0292 0.1056 1.0000
13.000 1.2117 0.03539 0.02833 0.0319 0.1035 1.0000
13.250 1.2143 0.03650 0.02956 0.0338 0.1012 1.0000
13.500 1.2222 0.03742 0.03050 0.0351 0.0990 1.0000
13.750 1.2410 0.03826 0.03120 0.0356 0.0966 1.0000
14.000 1.2365 0.04014 0.03328 0.0370 0.0946 1.0000
14.250 1.2303 0.04214 0.03550 0.0379 0.0925 1.0000
14.500 1.2313 0.04387 0.03730 0.0384 0.0903 1.0000
14.750 1.2421 0.04499 0.03837 0.0387 0.0882 1.0000
15.000 1.2507 0.04675 0.04012 0.0390 0.0860 1.0000
15.250 1.2373 0.05001 0.04364 0.0387 0.0844 1.0000
15.500 1.2275 0.05326 0.04708 0.0380 0.0826 1.0000
15.750 1.2269 0.05573 0.04962 0.0374 0.0808 1.0000
16.000 1.2417 0.05675 0.05054 0.0375 0.0789 1.0000
16.250 1.2397 0.05976 0.05362 0.0368 0.0773 1.0000
16.500 1.2167 0.06506 0.05920 0.0345 0.0763 1.0000
16.750 1.1943 0.07067 0.06506 0.0317 0.0751 1.0000
17.000 1.1724 0.07664 0.07123 0.0286 0.0739 1.0000
17.250 1.1543 0.08245 0.07720 0.0254 0.0728 1.0000
17.500 1.1667 0.08387 0.07856 0.0251 0.0713 1.0000
17.750 1.1845 0.08461 0.07920 0.0256 0.0699 1.0000
18.000 1.1286 0.09684 0.09180 0.0179 0.0696 1.0000
18.250 0.7083 0.20486 0.20057 -0.0464 0.0814 1.0000
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