GOE 679 AIRFOIL (goe679-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 679 AIRFOIL (goe679-il) Reynolds number: 1,000,000 Max Cl/Cd: 95.94 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe679-il-1000000.txt Download as CSV file: xf-goe679-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 679 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.7987 0.11539 0.11258 -0.0619 1.0000 0.0300
-19.000 -0.8198 0.10871 0.10579 -0.0653 1.0000 0.0300
-18.750 -0.8370 0.10281 0.09980 -0.0682 1.0000 0.0301
-18.500 -0.8516 0.09746 0.09436 -0.0707 1.0000 0.0302
-18.250 -0.8661 0.09231 0.08913 -0.0731 1.0000 0.0303
-18.000 -0.8791 0.08747 0.08421 -0.0752 1.0000 0.0304
-17.750 -0.8928 0.08262 0.07928 -0.0774 1.0000 0.0305
-17.500 -0.9049 0.07831 0.07490 -0.0791 1.0000 0.0305
-17.250 -0.9188 0.07388 0.07039 -0.0809 1.0000 0.0305
-17.000 -0.9344 0.06940 0.06584 -0.0826 1.0000 0.0306
-16.750 -0.9502 0.06502 0.06138 -0.0841 1.0000 0.0307
-16.500 -0.9563 0.06037 0.05665 -0.0877 0.9994 0.0307
-16.250 -0.9594 0.05556 0.05174 -0.0922 0.9982 0.0308
-16.000 -0.9594 0.05106 0.04714 -0.0966 0.9967 0.0308
-15.750 -0.9557 0.04662 0.04259 -0.1016 0.9951 0.0310
-15.500 -0.9490 0.04264 0.03850 -0.1064 0.9938 0.0311
-15.250 -0.9435 0.03862 0.03436 -0.1114 0.9928 0.0312
-15.000 -0.9496 0.03467 0.03031 -0.1139 0.9893 0.0314
-14.750 -0.9504 0.03124 0.02679 -0.1168 0.9863 0.0316
-14.500 -0.9399 0.02907 0.02453 -0.1188 0.9842 0.0317
-14.250 -0.9253 0.02731 0.02270 -0.1207 0.9826 0.0320
-14.000 -0.9060 0.02592 0.02126 -0.1223 0.9814 0.0322
-13.750 -0.9044 0.02482 0.02010 -0.1196 0.9760 0.0323
-13.500 -0.8890 0.02387 0.01910 -0.1191 0.9729 0.0326
-13.250 -0.8686 0.02301 0.01819 -0.1192 0.9710 0.0328
-13.000 -0.8456 0.02221 0.01734 -0.1195 0.9695 0.0331
-12.750 -0.8199 0.02147 0.01656 -0.1200 0.9684 0.0334
-12.500 -0.8188 0.02089 0.01594 -0.1155 0.9611 0.0336
-12.250 -0.7939 0.02012 0.01511 -0.1156 0.9587 0.0339
-12.000 -0.7650 0.01942 0.01437 -0.1163 0.9572 0.0342
-11.750 -0.7347 0.01876 0.01367 -0.1173 0.9562 0.0345
-11.500 -0.7032 0.01809 0.01296 -0.1185 0.9553 0.0348
-11.250 -0.6936 0.01763 0.01246 -0.1150 0.9483 0.0349
-11.000 -0.6677 0.01696 0.01174 -0.1149 0.9455 0.0352
-10.750 -0.6413 0.01608 0.01082 -0.1152 0.9436 0.0358
-10.500 -0.6093 0.01536 0.01009 -0.1163 0.9422 0.0364
-10.250 -0.5714 0.01469 0.00940 -0.1184 0.9408 0.0370
-10.000 -0.5622 0.01425 0.00893 -0.1145 0.9300 0.0374
-9.750 -0.5264 0.01368 0.00832 -0.1161 0.9264 0.0379
-9.500 -0.5114 0.01334 0.00794 -0.1134 0.9157 0.0384
-9.250 -0.4736 0.01288 0.00745 -0.1154 0.9110 0.0390
-9.000 -0.4457 0.01253 0.00705 -0.1154 0.9005 0.0394
-8.750 -0.4057 0.01194 0.00641 -0.1181 0.8914 0.0407
-8.500 -0.3662 0.01156 0.00598 -0.1205 0.8783 0.0417
-8.250 -0.3234 0.01125 0.00561 -0.1236 0.8640 0.0430
-8.000 -0.2884 0.01103 0.00528 -0.1250 0.8465 0.0442
-7.750 -0.2627 0.01078 0.00495 -0.1245 0.8286 0.0460
-7.500 -0.2396 0.01061 0.00471 -0.1234 0.8142 0.0480
-7.250 -0.2178 0.01042 0.00446 -0.1221 0.8018 0.0510
-7.000 -0.1974 0.01022 0.00424 -0.1204 0.7911 0.0551
-6.750 -0.1776 0.00996 0.00399 -0.1187 0.7808 0.0642
-6.500 -0.1588 0.00966 0.00375 -0.1168 0.7714 0.0802
-6.250 -0.1384 0.00948 0.00359 -0.1151 0.7618 0.0949
-6.000 -0.1167 0.00933 0.00347 -0.1137 0.7539 0.1049
-5.750 -0.0950 0.00923 0.00336 -0.1122 0.7453 0.1129
-5.500 -0.0729 0.00913 0.00327 -0.1108 0.7373 0.1191
-5.250 -0.0510 0.00906 0.00318 -0.1093 0.7285 0.1247
-5.000 -0.0293 0.00900 0.00309 -0.1078 0.7202 0.1297
-4.750 -0.0080 0.00891 0.00301 -0.1062 0.7120 0.1348
-4.500 0.0126 0.00890 0.00293 -0.1044 0.7032 0.1380
-4.250 0.0330 0.00879 0.00284 -0.1026 0.6951 0.1436
-4.000 0.0525 0.00875 0.00277 -0.1006 0.6849 0.1480
-3.750 0.0738 0.00872 0.00270 -0.0990 0.6751 0.1515
-3.500 0.0927 0.00866 0.00262 -0.0969 0.6640 0.1567
-3.250 0.1139 0.00861 0.00256 -0.0953 0.6529 0.1613
-3.000 0.1337 0.00862 0.00251 -0.0933 0.6401 0.1649
-2.750 0.1523 0.00859 0.00245 -0.0911 0.6246 0.1716
-2.500 0.1723 0.00859 0.00242 -0.0893 0.6091 0.1776
-2.250 0.1911 0.00862 0.00239 -0.0872 0.5919 0.1823
-2.000 0.2092 0.00864 0.00237 -0.0850 0.5735 0.1896
-1.750 0.2283 0.00872 0.00237 -0.0829 0.5553 0.1951
-1.500 0.2476 0.00878 0.00238 -0.0810 0.5382 0.2028
-1.250 0.2672 0.00885 0.00241 -0.0791 0.5224 0.2107
-1.000 0.2875 0.00893 0.00243 -0.0774 0.5075 0.2183
-0.750 0.3088 0.00898 0.00247 -0.0759 0.4945 0.2279
-0.500 0.3295 0.00905 0.00250 -0.0743 0.4824 0.2368
-0.250 0.3506 0.00910 0.00255 -0.0727 0.4719 0.2478
0.000 0.3717 0.00916 0.00259 -0.0712 0.4627 0.2583
0.250 0.3936 0.00920 0.00264 -0.0698 0.4546 0.2694
0.500 0.4140 0.00927 0.00270 -0.0681 0.4461 0.2816
1.000 0.4580 0.00936 0.00281 -0.0655 0.4322 0.3083
1.250 0.4793 0.00941 0.00287 -0.0640 0.4253 0.3227
1.500 0.5019 0.00943 0.00293 -0.0628 0.4200 0.3391
1.750 0.5224 0.00947 0.00300 -0.0612 0.4138 0.3615
2.000 0.5417 0.00951 0.00310 -0.0594 0.4076 0.3895
2.250 0.5627 0.00946 0.00317 -0.0579 0.4033 0.4293
2.500 0.5814 0.00940 0.00327 -0.0560 0.3978 0.4881
2.750 0.5958 0.00928 0.00340 -0.0533 0.3922 0.5830
3.000 0.6082 0.00907 0.00353 -0.0500 0.3877 0.6960
3.250 0.6187 0.00876 0.00368 -0.0461 0.3841 0.8359
3.500 0.7990 0.00919 0.00424 -0.0791 0.3697 0.9703
3.750 0.8374 0.00937 0.00441 -0.0813 0.3648 0.9840
4.000 0.8724 0.00961 0.00460 -0.0828 0.3588 0.9920
4.500 0.9566 0.01006 0.00494 -0.0890 0.3465 1.0000
4.750 0.9717 0.01018 0.00504 -0.0865 0.3410 1.0000
5.000 0.9850 0.01037 0.00518 -0.0836 0.3347 1.0000
5.250 1.0026 0.01048 0.00528 -0.0816 0.3302 1.0000
5.500 1.0198 0.01063 0.00541 -0.0795 0.3247 1.0000
5.750 1.0356 0.01085 0.00557 -0.0771 0.3184 1.0000
6.000 1.0538 0.01101 0.00572 -0.0753 0.3134 1.0000
6.250 1.0715 0.01120 0.00589 -0.0733 0.3077 1.0000
6.500 1.0874 0.01147 0.00611 -0.0711 0.3006 1.0000
6.750 1.1063 0.01167 0.00629 -0.0695 0.2942 1.0000
7.000 1.1243 0.01192 0.00651 -0.0677 0.2879 1.0000
7.250 1.1410 0.01222 0.00677 -0.0658 0.2806 1.0000
7.500 1.1595 0.01248 0.00701 -0.0642 0.2744 1.0000
7.750 1.1755 0.01285 0.00732 -0.0622 0.2666 1.0000
8.000 1.1948 0.01312 0.00759 -0.0608 0.2612 1.0000
8.250 1.2118 0.01347 0.00791 -0.0591 0.2550 1.0000
8.500 1.2281 0.01387 0.00827 -0.0573 0.2490 1.0000
8.750 1.2471 0.01418 0.00857 -0.0560 0.2441 1.0000
9.000 1.2638 0.01458 0.00896 -0.0543 0.2388 1.0000
9.250 1.2793 0.01505 0.00940 -0.0525 0.2335 1.0000
9.500 1.2984 0.01539 0.00975 -0.0513 0.2301 1.0000
9.750 1.3158 0.01580 0.01016 -0.0499 0.2264 1.0000
10.000 1.3308 0.01633 0.01066 -0.0482 0.2219 1.0000
10.250 1.3464 0.01685 0.01118 -0.0466 0.2179 1.0000
10.500 1.3645 0.01727 0.01162 -0.0454 0.2155 1.0000
10.750 1.3810 0.01777 0.01212 -0.0441 0.2117 1.0000
11.000 1.3959 0.01837 0.01271 -0.0426 0.2083 1.0000
11.250 1.4078 0.01913 0.01345 -0.0408 0.2038 1.0000
11.500 1.4258 0.01960 0.01397 -0.0398 0.2021 1.0000
11.750 1.4422 0.02016 0.01456 -0.0386 0.1998 1.0000
12.000 1.4578 0.02079 0.01520 -0.0374 0.1974 1.0000
12.250 1.4714 0.02155 0.01597 -0.0360 0.1948 1.0000
12.500 1.4841 0.02238 0.01681 -0.0347 0.1920 1.0000
12.750 1.4946 0.02336 0.01780 -0.0331 0.1891 1.0000
13.000 1.5117 0.02397 0.01845 -0.0323 0.1875 1.0000
13.250 1.5265 0.02473 0.01925 -0.0313 0.1855 1.0000
13.500 1.5404 0.02557 0.02012 -0.0303 0.1834 1.0000
13.750 1.5521 0.02658 0.02114 -0.0291 0.1811 1.0000
14.000 1.5626 0.02767 0.02226 -0.0279 0.1787 1.0000
14.250 1.5691 0.02907 0.02367 -0.0265 0.1759 1.0000
14.500 1.5836 0.02994 0.02459 -0.0257 0.1746 1.0000
14.750 1.5966 0.03094 0.02564 -0.0249 0.1731 1.0000
15.000 1.6091 0.03198 0.02672 -0.0241 0.1710 1.0000
15.250 1.6189 0.03325 0.02803 -0.0232 0.1690 1.0000
15.500 1.6270 0.03466 0.02946 -0.0223 0.1664 1.0000
15.750 1.6308 0.03645 0.03127 -0.0212 0.1635 1.0000
16.000 1.6405 0.03780 0.03266 -0.0204 0.1614 1.0000
16.250 1.6509 0.03911 0.03403 -0.0198 0.1595 1.0000
16.500 1.6597 0.04057 0.03553 -0.0192 0.1568 1.0000
16.750 1.6640 0.04245 0.03744 -0.0185 0.1540 1.0000
17.000 1.6627 0.04488 0.03988 -0.0176 0.1504 1.0000
17.250 1.6716 0.04641 0.04147 -0.0172 0.1485 1.0000
17.500 1.6775 0.04826 0.04338 -0.0167 0.1469 1.0000
17.750 1.6803 0.05043 0.04558 -0.0163 0.1432 1.0000
18.000 1.6795 0.05298 0.04817 -0.0159 0.1404 1.0000
18.250 1.6775 0.05572 0.05095 -0.0155 0.1376 1.0000
18.500 1.6808 0.05794 0.05324 -0.0153 0.1348 1.0000
18.750 1.6796 0.06066 0.05600 -0.0152 0.1314 1.0000
19.000 1.6689 0.06448 0.05985 -0.0151 0.1272 1.0000
19.250 1.6675 0.06731 0.06274 -0.0152 0.1233 1.0000
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