GOE 766 AIRFOIL (goe766-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 766 AIRFOIL (goe766-il) Reynolds number: 1,000,000 Max Cl/Cd: 87.22 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe766-il-1000000-n5.txt Download as CSV file: xf-goe766-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 766 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
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1636 0.10619 0.10344 -0.0119 1.0000 0.0170
-19.000 -1.2778 0.08261 0.07954 -0.0261 1.0000 0.0166
-18.750 -1.3425 0.06779 0.06446 -0.0354 1.0000 0.0164
-18.500 -1.3739 0.05888 0.05535 -0.0412 1.0000 0.0165
-18.250 -1.3950 0.05209 0.04839 -0.0455 1.0000 0.0166
-18.000 -1.4075 0.04702 0.04318 -0.0484 1.0000 0.0166
-17.750 -1.4142 0.04309 0.03912 -0.0502 1.0000 0.0168
-17.500 -1.4179 0.03977 0.03568 -0.0514 1.0000 0.0170
-17.250 -1.4178 0.03713 0.03293 -0.0520 1.0000 0.0171
-17.000 -1.4178 0.03466 0.03037 -0.0522 1.0000 0.0174
-16.750 -1.4160 0.03256 0.02818 -0.0519 1.0000 0.0176
-16.500 -1.4099 0.03099 0.02656 -0.0512 1.0000 0.0179
-16.250 -1.4040 0.02953 0.02502 -0.0503 1.0000 0.0182
-16.000 -1.3960 0.02831 0.02375 -0.0491 1.0000 0.0185
-15.750 -1.3876 0.02721 0.02257 -0.0477 1.0000 0.0187
-15.500 -1.3789 0.02620 0.02150 -0.0461 1.0000 0.0190
-15.250 -1.3690 0.02531 0.02054 -0.0443 1.0000 0.0193
-15.000 -1.3590 0.02448 0.01964 -0.0424 1.0000 0.0196
-14.750 -1.3484 0.02373 0.01881 -0.0403 1.0000 0.0198
-14.500 -1.3370 0.02307 0.01808 -0.0382 1.0000 0.0201
-14.250 -1.3252 0.02247 0.01741 -0.0359 1.0000 0.0203
-14.000 -1.3150 0.02183 0.01672 -0.0333 1.0000 0.0206
-13.750 -1.3029 0.02123 0.01609 -0.0309 1.0000 0.0209
-13.500 -1.2871 0.02068 0.01550 -0.0291 1.0000 0.0212
-13.250 -1.2699 0.02018 0.01497 -0.0274 1.0000 0.0216
-13.000 -1.2522 0.01970 0.01445 -0.0258 1.0000 0.0219
-12.750 -1.2339 0.01923 0.01394 -0.0243 1.0000 0.0222
-12.500 -1.2152 0.01877 0.01344 -0.0228 1.0000 0.0226
-12.250 -1.1957 0.01835 0.01297 -0.0214 1.0000 0.0230
-12.000 -1.1759 0.01795 0.01252 -0.0200 1.0000 0.0233
-11.750 -1.1559 0.01754 0.01206 -0.0185 1.0000 0.0236
-11.500 -1.1356 0.01715 0.01162 -0.0172 1.0000 0.0238
-11.250 -1.1168 0.01663 0.01106 -0.0156 1.0000 0.0242
-11.000 -1.0971 0.01617 0.01058 -0.0141 1.0000 0.0247
-10.750 -1.0767 0.01576 0.01016 -0.0127 1.0000 0.0250
-10.500 -1.0556 0.01540 0.00978 -0.0114 1.0000 0.0254
-10.250 -1.0345 0.01505 0.00940 -0.0101 1.0000 0.0258
-10.000 -1.0131 0.01472 0.00905 -0.0087 1.0000 0.0262
-9.750 -0.9917 0.01440 0.00871 -0.0074 1.0000 0.0266
-9.500 -0.9704 0.01408 0.00835 -0.0060 1.0000 0.0270
-9.250 -0.9492 0.01376 0.00800 -0.0046 1.0000 0.0273
-9.000 -0.9277 0.01347 0.00768 -0.0033 1.0000 0.0276
-8.750 -0.9014 0.01315 0.00734 -0.0029 0.9992 0.0280
-8.500 -0.8697 0.01270 0.00688 -0.0038 0.9964 0.0286
-8.250 -0.8398 0.01234 0.00652 -0.0042 0.9922 0.0291
-8.000 -0.8098 0.01203 0.00620 -0.0046 0.9871 0.0296
-7.500 -0.7481 0.01144 0.00559 -0.0057 0.9764 0.0308
-7.250 -0.7115 0.01115 0.00530 -0.0075 0.9703 0.0314
-7.000 -0.6744 0.01088 0.00500 -0.0094 0.9597 0.0320
-6.750 -0.6345 0.01056 0.00466 -0.0119 0.9448 0.0327
-6.500 -0.5979 0.01027 0.00434 -0.0136 0.9203 0.0338
-6.250 -0.5697 0.01012 0.00409 -0.0134 0.8871 0.0346
-6.000 -0.5456 0.01004 0.00388 -0.0123 0.8419 0.0354
-5.750 -0.5231 0.01003 0.00367 -0.0109 0.7836 0.0363
-5.500 -0.5003 0.01005 0.00348 -0.0096 0.7266 0.0371
-5.250 -0.4766 0.01002 0.00330 -0.0086 0.6797 0.0384
-5.000 -0.4525 0.00999 0.00313 -0.0076 0.6308 0.0400
-4.750 -0.4280 0.00999 0.00297 -0.0068 0.5826 0.0416
-4.500 -0.4026 0.00997 0.00282 -0.0061 0.5452 0.0431
-4.000 -0.3509 0.00981 0.00253 -0.0049 0.5006 0.0482
-3.750 -0.3244 0.00973 0.00240 -0.0044 0.4851 0.0508
-3.500 -0.2981 0.00961 0.00227 -0.0039 0.4725 0.0549
-3.250 -0.2716 0.00952 0.00216 -0.0034 0.4600 0.0596
-3.000 -0.2454 0.00942 0.00204 -0.0029 0.4475 0.0678
-2.750 -0.2192 0.00926 0.00192 -0.0024 0.4372 0.0821
-2.500 -0.1932 0.00911 0.00183 -0.0018 0.4282 0.1026
-2.250 -0.1667 0.00898 0.00176 -0.0014 0.4199 0.1206
-2.000 -0.1399 0.00891 0.00169 -0.0010 0.4117 0.1329
-1.750 -0.1128 0.00884 0.00164 -0.0006 0.4040 0.1431
-1.250 -0.0590 0.00870 0.00153 0.0002 0.3866 0.1675
-0.750 -0.0072 0.00838 0.00141 0.0013 0.3703 0.2398
-0.500 0.0166 0.00803 0.00134 0.0021 0.3619 0.3293
-0.250 0.0417 0.00781 0.00130 0.0028 0.3542 0.3917
0.000 0.0668 0.00762 0.00127 0.0035 0.3450 0.4469
0.250 0.0904 0.00733 0.00125 0.0045 0.3368 0.5335
0.500 0.1153 0.00721 0.00125 0.0052 0.3269 0.5889
0.750 0.1414 0.00716 0.00127 0.0058 0.3164 0.6207
1.000 0.1672 0.00713 0.00130 0.0064 0.3057 0.6533
1.250 0.1924 0.00709 0.00133 0.0072 0.2950 0.6905
1.500 0.2177 0.00704 0.00137 0.0080 0.2869 0.7265
1.750 0.2435 0.00705 0.00142 0.0086 0.2781 0.7514
2.000 0.2694 0.00704 0.00147 0.0093 0.2716 0.7762
2.250 0.2950 0.00706 0.00153 0.0100 0.2636 0.8029
2.500 0.3208 0.00706 0.00161 0.0107 0.2576 0.8288
2.750 0.3467 0.00707 0.00169 0.0114 0.2511 0.8584
3.000 0.3732 0.00712 0.00178 0.0119 0.2437 0.8875
3.250 0.4023 0.00718 0.00188 0.0119 0.2362 0.9113
3.500 0.4360 0.00730 0.00202 0.0109 0.2296 0.9323
3.750 0.4719 0.00741 0.00214 0.0094 0.2247 0.9456
4.000 0.5062 0.00759 0.00226 0.0081 0.2155 0.9542
4.250 0.5413 0.00773 0.00238 0.0067 0.2088 0.9605
4.500 0.5758 0.00787 0.00250 0.0053 0.2031 0.9655
4.750 0.6053 0.00803 0.00262 0.0051 0.1972 0.9711
5.000 0.6389 0.00816 0.00275 0.0040 0.1921 0.9733
5.250 0.6706 0.00835 0.00288 0.0032 0.1841 0.9760
5.500 0.7009 0.00850 0.00302 0.0028 0.1768 0.9795
5.750 0.7292 0.00871 0.00317 0.0027 0.1672 0.9830
6.000 0.7616 0.00894 0.00334 0.0017 0.1546 0.9847
6.250 0.7929 0.00923 0.00355 0.0009 0.1392 0.9867
6.500 0.8231 0.00957 0.00380 0.0003 0.1226 0.9890
6.750 0.8525 0.00989 0.00406 -0.0002 0.1103 0.9914
7.000 0.8813 0.01021 0.00432 -0.0005 0.1003 0.9936
7.250 0.9125 0.01054 0.00460 -0.0014 0.0907 0.9952
7.500 0.9432 0.01087 0.00488 -0.0021 0.0822 0.9969
7.750 0.9741 0.01118 0.00516 -0.0029 0.0752 0.9984
8.000 1.0048 0.01152 0.00546 -0.0037 0.0685 0.9996
8.250 1.0295 0.01183 0.00576 -0.0032 0.0642 1.0000
8.500 1.0505 0.01213 0.00605 -0.0020 0.0607 1.0000
8.750 1.0720 0.01240 0.00633 -0.0007 0.0582 1.0000
9.000 1.0930 0.01271 0.00664 0.0005 0.0558 1.0000
9.250 1.1136 0.01306 0.00698 0.0018 0.0531 1.0000
9.500 1.1351 0.01334 0.00728 0.0030 0.0518 1.0000
9.750 1.1562 0.01364 0.00760 0.0042 0.0500 1.0000
10.000 1.1767 0.01399 0.00796 0.0055 0.0483 1.0000
10.250 1.1967 0.01438 0.00835 0.0068 0.0465 1.0000
10.500 1.2172 0.01472 0.00872 0.0080 0.0454 1.0000
10.750 1.2378 0.01505 0.00908 0.0092 0.0444 1.0000
11.000 1.2579 0.01541 0.00946 0.0105 0.0434 1.0000
11.250 1.2774 0.01580 0.00988 0.0118 0.0422 1.0000
11.500 1.2962 0.01625 0.01034 0.0132 0.0410 1.0000
11.750 1.3141 0.01673 0.01084 0.0147 0.0397 1.0000
12.000 1.3330 0.01713 0.01129 0.0160 0.0392 1.0000
12.250 1.3515 0.01754 0.01174 0.0174 0.0384 1.0000
12.500 1.3690 0.01799 0.01222 0.0189 0.0375 1.0000
12.750 1.3854 0.01848 0.01274 0.0205 0.0364 1.0000
13.000 1.4001 0.01903 0.01332 0.0223 0.0354 1.0000
13.250 1.4125 0.01965 0.01397 0.0244 0.0344 1.0000
13.500 1.4228 0.02018 0.01455 0.0270 0.0340 1.0000
13.750 1.4336 0.02072 0.01515 0.0293 0.0334 1.0000
14.000 1.4437 0.02138 0.01585 0.0315 0.0327 1.0000
14.250 1.4533 0.02213 0.01665 0.0334 0.0320 1.0000
14.500 1.4620 0.02302 0.01761 0.0352 0.0316 1.0000
14.750 1.4696 0.02408 0.01872 0.0367 0.0311 1.0000
15.000 1.4755 0.02539 0.02008 0.0379 0.0304 1.0000
15.250 1.4797 0.02699 0.02175 0.0387 0.0298 1.0000
15.500 1.4843 0.02877 0.02361 0.0391 0.0294 1.0000
15.750 1.4883 0.03084 0.02577 0.0389 0.0290 1.0000
16.000 1.4916 0.03323 0.02826 0.0382 0.0286 1.0000
16.250 1.4919 0.03616 0.03129 0.0371 0.0281 1.0000
16.500 1.4899 0.03955 0.03477 0.0356 0.0277 1.0000
16.750 1.4844 0.04346 0.03878 0.0338 0.0272 1.0000
17.000 1.4744 0.04798 0.04341 0.0317 0.0269 1.0000
17.250 1.4617 0.05282 0.04837 0.0296 0.0268 1.0000
17.500 1.4447 0.05819 0.05383 0.0273 0.0263 1.0000
17.750 1.4256 0.06380 0.05956 0.0250 0.0262 1.0000
18.000 1.4045 0.06978 0.06566 0.0224 0.0261 1.0000
18.250 1.3825 0.07606 0.07203 0.0197 0.0257 1.0000
18.500 1.3634 0.08215 0.07823 0.0169 0.0257 1.0000
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