GOE 617 AIRFOIL (goe617-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 617 AIRFOIL (goe617-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.97 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe617-il-1000000.txt Download as CSV file: xf-goe617-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 617 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 -0.8456 0.13161 0.12935 -0.0285 1.0000 0.0164
-19.000 -0.9047 0.11607 0.11363 -0.0371 1.0000 0.0164
-18.750 -0.9529 0.10347 0.10088 -0.0443 1.0000 0.0163
-18.500 -1.0010 0.09146 0.08873 -0.0511 1.0000 0.0163
-18.250 -1.0526 0.07908 0.07617 -0.0583 1.0000 0.0161
-18.000 -1.0935 0.06853 0.06543 -0.0646 1.0000 0.0161
-17.750 -1.1238 0.06002 0.05675 -0.0699 1.0000 0.0161
-17.500 -1.1437 0.05345 0.05003 -0.0740 1.0000 0.0162
-17.250 -1.1605 0.04773 0.04415 -0.0773 1.0000 0.0162
-17.000 -1.1649 0.04405 0.04035 -0.0791 1.0000 0.0164
-16.750 -1.1743 0.04016 0.03633 -0.0805 1.0000 0.0165
-16.500 -1.1743 0.03762 0.03367 -0.0810 1.0000 0.0167
-16.250 -1.1856 0.03435 0.03028 -0.0808 1.0000 0.0169
-16.000 -1.1903 0.03200 0.02785 -0.0799 1.0000 0.0173
-15.750 -1.1904 0.03024 0.02602 -0.0786 1.0000 0.0175
-15.500 -1.1873 0.02883 0.02455 -0.0770 1.0000 0.0178
-15.250 -1.1783 0.02792 0.02360 -0.0755 1.0000 0.0182
-15.000 -1.1727 0.02687 0.02247 -0.0735 1.0000 0.0184
-14.750 -1.1663 0.02594 0.02147 -0.0714 1.0000 0.0188
-14.500 -1.1581 0.02518 0.02065 -0.0691 1.0000 0.0192
-14.250 -1.1508 0.02444 0.01984 -0.0666 1.0000 0.0195
-14.000 -1.1415 0.02387 0.01919 -0.0641 1.0000 0.0198
-13.750 -1.1338 0.02328 0.01852 -0.0613 1.0000 0.0200
-13.500 -1.1393 0.02222 0.01740 -0.0564 1.0000 0.0204
-13.250 -1.1412 0.02155 0.01668 -0.0516 1.0000 0.0208
-13.000 -1.1428 0.02113 0.01623 -0.0465 1.0000 0.0211
-12.750 -1.1455 0.02085 0.01591 -0.0410 1.0000 0.0214
-12.500 -1.1363 0.02054 0.01558 -0.0379 0.9997 0.0218
-12.250 -1.1062 0.01995 0.01494 -0.0390 0.9982 0.0224
-12.000 -1.0747 0.01955 0.01449 -0.0402 0.9965 0.0232
-11.750 -1.0428 0.01912 0.01399 -0.0415 0.9948 0.0237
-11.500 -1.0166 0.01812 0.01292 -0.0421 0.9924 0.0245
-11.250 -0.9891 0.01747 0.01225 -0.0426 0.9893 0.0252
-11.000 -0.9582 0.01697 0.01174 -0.0436 0.9868 0.0259
-10.750 -0.9250 0.01650 0.01123 -0.0451 0.9847 0.0268
-10.500 -0.8904 0.01606 0.01074 -0.0468 0.9830 0.0275
-10.250 -0.8606 0.01573 0.01036 -0.0474 0.9791 0.0281
-10.000 -0.8352 0.01483 0.00941 -0.0475 0.9746 0.0292
-9.750 -0.8044 0.01429 0.00886 -0.0484 0.9721 0.0300
-9.500 -0.7713 0.01385 0.00839 -0.0498 0.9701 0.0310
-9.250 -0.7429 0.01350 0.00802 -0.0501 0.9647 0.0319
-9.000 -0.7102 0.01316 0.00763 -0.0513 0.9607 0.0328
-8.750 -0.6763 0.01257 0.00700 -0.0529 0.9576 0.0340
-8.500 -0.6434 0.01209 0.00653 -0.0542 0.9530 0.0354
-8.250 -0.6122 0.01176 0.00617 -0.0551 0.9464 0.0366
-8.000 -0.5773 0.01142 0.00579 -0.0567 0.9411 0.0378
-7.750 -0.5485 0.01117 0.00549 -0.0570 0.9328 0.0388
-7.500 -0.5196 0.01075 0.00505 -0.0574 0.9251 0.0411
-7.250 -0.4946 0.01052 0.00480 -0.0568 0.9158 0.0429
-6.750 -0.4442 0.01009 0.00431 -0.0557 0.8997 0.0474
-6.500 -0.4184 0.00992 0.00412 -0.0552 0.8919 0.0506
-6.250 -0.3948 0.00977 0.00395 -0.0543 0.8838 0.0537
-6.000 -0.3701 0.00960 0.00380 -0.0536 0.8763 0.0579
-5.750 -0.3451 0.00953 0.00369 -0.0529 0.8687 0.0608
-5.500 -0.3212 0.00935 0.00350 -0.0520 0.8608 0.0649
-5.250 -0.2965 0.00924 0.00339 -0.0512 0.8533 0.0684
-5.000 -0.2714 0.00916 0.00327 -0.0506 0.8452 0.0708
-4.750 -0.2469 0.00903 0.00311 -0.0497 0.8372 0.0733
-4.500 -0.2235 0.00885 0.00291 -0.0487 0.8283 0.0770
-4.250 -0.1991 0.00873 0.00276 -0.0479 0.8196 0.0799
-4.000 -0.1747 0.00864 0.00263 -0.0471 0.8093 0.0822
-3.750 -0.1502 0.00856 0.00250 -0.0462 0.7979 0.0841
-3.500 -0.1268 0.00841 0.00233 -0.0452 0.7859 0.0890
-3.250 -0.1031 0.00830 0.00219 -0.0442 0.7739 0.0931
-3.000 -0.0788 0.00821 0.00208 -0.0433 0.7616 0.0979
-2.750 -0.0557 0.00805 0.00196 -0.0423 0.7485 0.1132
-2.500 -0.0352 0.00774 0.00186 -0.0408 0.7346 0.1732
-2.250 -0.0123 0.00762 0.00178 -0.0397 0.7199 0.2019
-2.000 0.0103 0.00750 0.00169 -0.0385 0.7043 0.2262
-1.750 0.0312 0.00729 0.00159 -0.0370 0.6885 0.2715
-1.500 0.0483 0.00690 0.00152 -0.0349 0.6739 0.3800
-1.250 0.0693 0.00674 0.00147 -0.0334 0.6598 0.4312
-1.000 0.0899 0.00656 0.00143 -0.0318 0.6465 0.4873
-0.750 0.1087 0.00634 0.00140 -0.0299 0.6338 0.5550
-0.500 0.1260 0.00613 0.00138 -0.0276 0.6198 0.6241
-0.250 0.1421 0.00593 0.00137 -0.0250 0.6060 0.6929
0.000 0.1576 0.00574 0.00138 -0.0221 0.5944 0.7649
0.250 0.1779 0.00563 0.00143 -0.0202 0.5846 0.8213
0.500 0.2015 0.00564 0.00150 -0.0191 0.5751 0.8579
0.750 0.2288 0.00567 0.00156 -0.0188 0.5655 0.8794
1.000 0.2560 0.00574 0.00162 -0.0185 0.5555 0.8949
1.250 0.2822 0.00583 0.00168 -0.0180 0.5442 0.9084
1.500 0.3120 0.00593 0.00177 -0.0183 0.5330 0.9216
1.750 0.3454 0.00606 0.00188 -0.0194 0.5226 0.9298
2.000 0.3699 0.00617 0.00196 -0.0185 0.5131 0.9399
2.250 0.4071 0.00632 0.00208 -0.0205 0.5032 0.9437
2.500 0.4389 0.00648 0.00219 -0.0213 0.4931 0.9480
2.750 0.4649 0.00662 0.00230 -0.0207 0.4827 0.9554
3.000 0.5036 0.00682 0.00245 -0.0231 0.4680 0.9573
3.250 0.5401 0.00703 0.00258 -0.0250 0.4499 0.9588
3.500 0.5742 0.00725 0.00272 -0.0264 0.4320 0.9606
3.750 0.6088 0.00748 0.00289 -0.0279 0.4171 0.9632
4.000 0.6327 0.00770 0.00306 -0.0270 0.4018 0.9694
4.250 0.6717 0.00800 0.00325 -0.0295 0.3811 0.9705
4.500 0.7090 0.00825 0.00343 -0.0317 0.3647 0.9718
5.000 0.7798 0.00877 0.00380 -0.0352 0.3308 0.9756
5.250 0.8101 0.00901 0.00398 -0.0359 0.3146 0.9784
5.500 0.8329 0.00926 0.00417 -0.0350 0.2986 0.9823
5.750 0.8660 0.00952 0.00433 -0.0364 0.2758 0.9833
6.000 0.8961 0.00995 0.00457 -0.0373 0.2383 0.9846
6.250 0.9229 0.01057 0.00493 -0.0377 0.1893 0.9864
6.500 0.9512 0.01096 0.00521 -0.0382 0.1709 0.9883
6.750 0.9794 0.01125 0.00546 -0.0386 0.1607 0.9904
7.000 1.0058 0.01155 0.00573 -0.0386 0.1525 0.9927
7.250 1.0350 0.01178 0.00595 -0.0392 0.1452 0.9941
7.500 1.0653 0.01206 0.00618 -0.0402 0.1363 0.9953
7.750 1.0957 0.01230 0.00640 -0.0411 0.1273 0.9967
8.000 1.1245 0.01262 0.00666 -0.0417 0.1153 0.9983
8.250 1.1526 0.01298 0.00695 -0.0423 0.1038 0.9996
8.500 1.1693 0.01331 0.00723 -0.0404 0.0962 1.0000
8.750 1.1801 0.01358 0.00750 -0.0373 0.0914 1.0000
9.000 1.1893 0.01386 0.00778 -0.0338 0.0878 1.0000
9.250 1.1950 0.01418 0.00808 -0.0297 0.0839 1.0000
9.500 1.1973 0.01437 0.00830 -0.0248 0.0815 1.0000
9.750 1.2019 0.01458 0.00855 -0.0204 0.0799 1.0000
10.000 1.2078 0.01485 0.00883 -0.0163 0.0779 1.0000
10.250 1.2146 0.01519 0.00918 -0.0126 0.0757 1.0000
10.500 1.2212 0.01562 0.00961 -0.0089 0.0729 1.0000
10.750 1.2312 0.01599 0.01002 -0.0060 0.0710 1.0000
11.000 1.2438 0.01632 0.01039 -0.0036 0.0696 1.0000
11.250 1.2556 0.01673 0.01083 -0.0011 0.0679 1.0000
11.500 1.2666 0.01721 0.01132 0.0013 0.0659 1.0000
11.750 1.2768 0.01777 0.01189 0.0038 0.0638 1.0000
12.000 1.2864 0.01841 0.01256 0.0062 0.0615 1.0000
12.250 1.3008 0.01886 0.01306 0.0079 0.0604 1.0000
12.500 1.3137 0.01942 0.01365 0.0097 0.0587 1.0000
12.750 1.3255 0.02008 0.01432 0.0115 0.0567 1.0000
13.000 1.3356 0.02087 0.01512 0.0133 0.0541 1.0000
13.250 1.3476 0.02160 0.01589 0.0149 0.0523 1.0000
13.500 1.3604 0.02231 0.01665 0.0163 0.0501 1.0000
13.750 1.3700 0.02326 0.01759 0.0178 0.0471 1.0000
14.000 1.3801 0.02422 0.01858 0.0193 0.0440 1.0000
14.250 1.3874 0.02542 0.01976 0.0208 0.0394 1.0000
14.500 1.3909 0.02693 0.02124 0.0224 0.0325 1.0000
14.750 1.3899 0.02887 0.02315 0.0241 0.0250 1.0000
15.000 1.3902 0.03081 0.02511 0.0255 0.0215 1.0000
15.250 1.3891 0.03298 0.02730 0.0267 0.0189 1.0000
15.500 1.3890 0.03517 0.02954 0.0277 0.0175 1.0000
15.750 1.3887 0.03747 0.03191 0.0284 0.0164 1.0000
16.000 1.3926 0.03947 0.03398 0.0289 0.0161 1.0000
16.250 1.3930 0.04189 0.03648 0.0292 0.0153 1.0000
16.500 1.3907 0.04467 0.03933 0.0294 0.0147 1.0000
16.750 1.3895 0.04742 0.04216 0.0295 0.0144 1.0000
17.000 1.3836 0.05079 0.04561 0.0293 0.0139 1.0000
17.250 1.3802 0.05399 0.04890 0.0290 0.0136 1.0000
17.500 1.3783 0.05705 0.05205 0.0285 0.0134 1.0000
17.750 1.3743 0.06045 0.05555 0.0279 0.0132 1.0000
18.000 1.3703 0.06393 0.05912 0.0272 0.0130 1.0000
18.250 1.3639 0.06778 0.06307 0.0263 0.0128 1.0000
18.500 1.3585 0.07156 0.06694 0.0253 0.0126 1.0000
18.750 1.3484 0.07608 0.07156 0.0240 0.0123 1.0000
19.000 1.3375 0.08084 0.07641 0.0224 0.0122 1.0000
19.250 1.3268 0.08563 0.08130 0.0208 0.0121 1.0000
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