GOE 775 AIRFOIL (goe775-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 775 AIRFOIL (goe775-il) Reynolds number: 1,000,000 Max Cl/Cd: 74.57 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe775-il-1000000.txt Download as CSV file: xf-goe775-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 775 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3313 0.08086 0.07626 -0.0371 1.0000 0.0527
-19.500 -1.3371 0.07701 0.07233 -0.0383 1.0000 0.0534
-19.250 -1.3443 0.07304 0.06828 -0.0394 1.0000 0.0541
-19.000 -1.3562 0.06856 0.06374 -0.0406 1.0000 0.0550
-18.750 -1.3643 0.06460 0.05971 -0.0416 1.0000 0.0560
-18.500 -1.3695 0.06102 0.05607 -0.0424 1.0000 0.0569
-18.250 -1.3725 0.05776 0.05275 -0.0430 1.0000 0.0579
-18.000 -1.3727 0.05484 0.04975 -0.0435 1.0000 0.0589
-17.750 -1.3764 0.05159 0.04644 -0.0440 1.0000 0.0600
-17.500 -1.3800 0.04843 0.04323 -0.0444 1.0000 0.0613
-17.250 -1.3801 0.04571 0.04047 -0.0446 1.0000 0.0626
-17.000 -1.3767 0.04337 0.03808 -0.0447 1.0000 0.0640
-16.750 -1.3720 0.04121 0.03585 -0.0447 1.0000 0.0653
-16.500 -1.3716 0.03868 0.03329 -0.0446 1.0000 0.0670
-16.250 -1.3679 0.03653 0.03111 -0.0444 1.0000 0.0687
-16.000 -1.3608 0.03473 0.02926 -0.0441 1.0000 0.0703
-15.750 -1.3531 0.03303 0.02752 -0.0438 1.0000 0.0720
-15.500 -1.3476 0.03119 0.02567 -0.0433 1.0000 0.0740
-15.250 -1.3392 0.02967 0.02412 -0.0427 1.0000 0.0760
-15.000 -1.3278 0.02841 0.02281 -0.0422 1.0000 0.0779
-14.750 -1.3198 0.02695 0.02133 -0.0414 1.0000 0.0801
-14.500 -1.3097 0.02570 0.02008 -0.0405 1.0000 0.0824
-14.250 -1.2968 0.02470 0.01905 -0.0397 1.0000 0.0846
-14.000 -1.2856 0.02363 0.01796 -0.0387 1.0000 0.0869
-13.750 -1.2745 0.02261 0.01694 -0.0376 1.0000 0.0894
-13.500 -1.2609 0.02180 0.01611 -0.0365 1.0000 0.0918
-13.250 -1.2470 0.02107 0.01535 -0.0353 1.0000 0.0938
-13.000 -1.2365 0.02021 0.01450 -0.0336 1.0000 0.0964
-12.750 -1.2251 0.01952 0.01380 -0.0318 1.0000 0.0988
-12.500 -1.2136 0.01898 0.01324 -0.0297 1.0000 0.1008
-12.250 -1.2065 0.01846 0.01270 -0.0269 1.0000 0.1029
-12.000 -1.2072 0.01795 0.01219 -0.0225 1.0000 0.1051
-11.750 -1.2057 0.01754 0.01178 -0.0185 0.9996 0.1073
-11.500 -1.1773 0.01703 0.01126 -0.0195 0.9979 0.1103
-11.250 -1.1504 0.01643 0.01067 -0.0203 0.9958 0.1141
-11.000 -1.1220 0.01589 0.01015 -0.0212 0.9939 0.1179
-10.750 -1.0917 0.01544 0.00969 -0.0224 0.9924 0.1215
-10.500 -1.0639 0.01489 0.00918 -0.0232 0.9905 0.1266
-10.250 -1.0359 0.01447 0.00876 -0.0238 0.9872 0.1310
-10.000 -1.0083 0.01394 0.00828 -0.0244 0.9840 0.1375
-9.750 -0.9792 0.01351 0.00788 -0.0252 0.9807 0.1439
-9.500 -0.9507 0.01304 0.00746 -0.0259 0.9776 0.1521
-9.250 -0.9308 0.01265 0.00711 -0.0246 0.9698 0.1596
-8.750 -0.8877 0.01195 0.00647 -0.0226 0.9561 0.1757
-8.500 -0.8670 0.01167 0.00619 -0.0212 0.9485 0.1828
-8.250 -0.8479 0.01139 0.00594 -0.0195 0.9404 0.1906
-8.000 -0.8282 0.01118 0.00572 -0.0179 0.9319 0.1970
-7.750 -0.8075 0.01093 0.00549 -0.0165 0.9240 0.2047
-7.500 -0.7843 0.01075 0.00530 -0.0155 0.9158 0.2110
-7.250 -0.7620 0.01050 0.00507 -0.0145 0.9079 0.2192
-7.000 -0.7376 0.01034 0.00491 -0.0138 0.9000 0.2257
-6.750 -0.7148 0.01009 0.00469 -0.0128 0.8911 0.2345
-6.500 -0.6897 0.00994 0.00453 -0.0122 0.8825 0.2417
-6.250 -0.6660 0.00971 0.00433 -0.0113 0.8723 0.2507
-6.000 -0.6406 0.00957 0.00417 -0.0108 0.8621 0.2585
-5.750 -0.6162 0.00937 0.00399 -0.0100 0.8497 0.2679
-5.500 -0.5905 0.00923 0.00385 -0.0095 0.8360 0.2763
-5.250 -0.5661 0.00906 0.00367 -0.0088 0.8193 0.2867
-4.750 -0.5160 0.00883 0.00338 -0.0075 0.7785 0.3059
-4.500 -0.4904 0.00878 0.00327 -0.0069 0.7580 0.3153
-4.000 -0.4392 0.00862 0.00307 -0.0058 0.7244 0.3356
-3.750 -0.4135 0.00854 0.00298 -0.0054 0.7104 0.3461
-3.500 -0.3872 0.00849 0.00290 -0.0049 0.6968 0.3558
-3.250 -0.3608 0.00840 0.00283 -0.0046 0.6852 0.3666
-2.750 -0.3075 0.00828 0.00270 -0.0039 0.6615 0.3867
-2.500 -0.2814 0.00824 0.00264 -0.0035 0.6491 0.3984
-2.250 -0.2542 0.00816 0.00259 -0.0032 0.6380 0.4111
-2.000 -0.2284 0.00810 0.00253 -0.0028 0.6254 0.4234
-1.750 -0.2008 0.00808 0.00249 -0.0026 0.6127 0.4327
-1.500 -0.1746 0.00802 0.00245 -0.0022 0.6003 0.4443
-1.000 -0.1208 0.00795 0.00238 -0.0016 0.5758 0.4662
-0.750 -0.0937 0.00796 0.00236 -0.0013 0.5631 0.4764
-0.500 -0.0669 0.00791 0.00234 -0.0010 0.5515 0.4893
-0.250 -0.0404 0.00792 0.00232 -0.0006 0.5382 0.5011
0.000 -0.0132 0.00790 0.00232 -0.0004 0.5262 0.5138
0.250 0.0134 0.00790 0.00232 0.0000 0.5144 0.5255
0.500 0.0407 0.00792 0.00232 0.0002 0.5021 0.5376
0.750 0.0671 0.00791 0.00234 0.0006 0.4902 0.5508
1.000 0.0940 0.00796 0.00236 0.0009 0.4774 0.5625
1.250 0.1210 0.00795 0.00238 0.0012 0.4671 0.5751
1.500 0.1476 0.00801 0.00241 0.0016 0.4554 0.5867
1.750 0.1748 0.00802 0.00244 0.0018 0.4453 0.5997
2.250 0.2286 0.00810 0.00253 0.0024 0.4244 0.6249
2.500 0.2544 0.00816 0.00259 0.0029 0.4119 0.6375
2.750 0.2817 0.00823 0.00263 0.0031 0.3995 0.6487
3.000 0.3077 0.00828 0.00270 0.0036 0.3877 0.6611
3.500 0.3610 0.00840 0.00282 0.0042 0.3676 0.6848
3.750 0.3876 0.00848 0.00290 0.0045 0.3569 0.6966
4.000 0.4137 0.00853 0.00297 0.0050 0.3472 0.7102
4.250 0.4396 0.00861 0.00306 0.0054 0.3368 0.7241
4.750 0.4908 0.00876 0.00326 0.0065 0.3165 0.7578
5.000 0.5163 0.00883 0.00338 0.0071 0.3070 0.7784
5.250 0.5407 0.00895 0.00353 0.0078 0.2964 0.7998
5.500 0.5664 0.00905 0.00367 0.0083 0.2878 0.8193
5.750 0.5907 0.00923 0.00384 0.0091 0.2771 0.8360
6.000 0.6166 0.00936 0.00398 0.0096 0.2689 0.8497
6.250 0.6408 0.00956 0.00417 0.0103 0.2593 0.8622
6.500 0.6664 0.00970 0.00432 0.0109 0.2517 0.8724
7.000 0.7152 0.01008 0.00468 0.0123 0.2355 0.8911
7.250 0.7382 0.01032 0.00489 0.0132 0.2269 0.8999
7.500 0.7625 0.01049 0.00506 0.0140 0.2203 0.9079
7.750 0.7851 0.01073 0.00529 0.0150 0.2123 0.9158
8.000 0.8080 0.01092 0.00549 0.0160 0.2057 0.9241
8.250 0.8290 0.01116 0.00571 0.0173 0.1981 0.9319
8.500 0.8486 0.01138 0.00593 0.0190 0.1915 0.9404
8.750 0.8679 0.01165 0.00618 0.0206 0.1839 0.9485
9.000 0.8884 0.01194 0.00646 0.0220 0.1766 0.9562
9.250 0.9077 0.01229 0.00677 0.0235 0.1683 0.9640
9.500 0.9316 0.01264 0.00710 0.0240 0.1604 0.9699
9.750 0.9517 0.01303 0.00745 0.0252 0.1528 0.9776
10.000 0.9804 0.01348 0.00785 0.0245 0.1447 0.9808
10.250 1.0093 0.01392 0.00827 0.0238 0.1382 0.9841
10.500 1.0371 0.01444 0.00874 0.0231 0.1317 0.9873
10.750 1.0649 0.01487 0.00916 0.0225 0.1271 0.9906
11.000 1.0931 0.01541 0.00966 0.0216 0.1221 0.9925
11.250 1.1233 0.01588 0.01013 0.0205 0.1184 0.9940
11.500 1.1519 0.01640 0.01064 0.0195 0.1146 0.9959
11.750 1.1785 0.01702 0.01124 0.0187 0.1107 0.9980
12.000 1.2072 0.01751 0.01175 0.0177 0.1078 0.9997
12.250 1.2071 0.01789 0.01214 0.0221 0.1057 1.0000
12.500 1.2074 0.01839 0.01263 0.0262 0.1035 1.0000
12.750 1.2138 0.01896 0.01321 0.0292 0.1013 1.0000
13.000 1.2260 0.01948 0.01376 0.0311 0.0993 1.0000
13.250 1.2381 0.02015 0.01444 0.0328 0.0969 1.0000
13.500 1.2492 0.02098 0.01526 0.0344 0.0944 1.0000
13.750 1.2623 0.02176 0.01607 0.0357 0.0923 1.0000
14.000 1.2765 0.02254 0.01687 0.0367 0.0899 1.0000
14.250 1.2881 0.02354 0.01787 0.0378 0.0875 1.0000
14.500 1.2986 0.02466 0.01900 0.0389 0.0851 1.0000
14.750 1.3122 0.02561 0.01999 0.0396 0.0830 1.0000
15.000 1.3229 0.02682 0.02121 0.0404 0.0807 1.0000
15.250 1.3305 0.02832 0.02272 0.0412 0.0784 1.0000
15.500 1.3420 0.02957 0.02401 0.0418 0.0766 1.0000
15.750 1.3512 0.03103 0.02551 0.0423 0.0745 1.0000
16.000 1.3574 0.03280 0.02729 0.0428 0.0725 1.0000
16.250 1.3641 0.03459 0.02912 0.0431 0.0707 1.0000
16.500 1.3717 0.03636 0.03093 0.0434 0.0691 1.0000
16.750 1.3762 0.03843 0.03304 0.0436 0.0674 1.0000
17.000 1.3772 0.04089 0.03553 0.0437 0.0657 1.0000
17.250 1.3811 0.04314 0.03783 0.0436 0.0643 1.0000
17.500 1.3851 0.04542 0.04017 0.0435 0.0629 1.0000
17.750 1.3852 0.04812 0.04292 0.0433 0.0615 1.0000
18.000 1.3820 0.05124 0.04608 0.0430 0.0602 1.0000
18.250 1.3777 0.05455 0.04945 0.0425 0.0590 1.0000
18.500 1.3781 0.05742 0.05239 0.0420 0.0581 1.0000
18.750 1.3756 0.06062 0.05566 0.0413 0.0570 1.0000
19.000 1.3707 0.06415 0.05925 0.0405 0.0560 1.0000
19.250 1.3630 0.06808 0.06325 0.0396 0.0551 1.0000
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