GOE 420 AIRFOIL (goe420-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 420 AIRFOIL (goe420-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.2 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe420-il-1000000-n5.txt Download as CSV file: xf-goe420-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 420 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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7792 0.11327 0.11020 -0.0696 1.0000 0.0233
-19.500 -0.7859 0.10868 0.10554 -0.0721 1.0000 0.0233
-19.250 -0.7938 0.10387 0.10067 -0.0747 1.0000 0.0235
-19.000 -0.8013 0.09924 0.09597 -0.0772 1.0000 0.0235
-18.750 -0.8069 0.09499 0.09166 -0.0794 1.0000 0.0236
-18.500 -0.8136 0.09061 0.08722 -0.0817 1.0000 0.0237
-18.250 -0.8199 0.08641 0.08296 -0.0839 1.0000 0.0237
-18.000 -0.8259 0.08229 0.07877 -0.0860 1.0000 0.0239
-17.750 -0.8326 0.07817 0.07459 -0.0881 1.0000 0.0239
-17.500 -0.8381 0.07431 0.07067 -0.0899 1.0000 0.0240
-17.250 -0.8444 0.07041 0.06671 -0.0918 1.0000 0.0241
-17.000 -0.8526 0.06642 0.06266 -0.0936 1.0000 0.0241
-16.750 -0.8530 0.06256 0.05873 -0.0960 0.9906 0.0242
-16.500 -0.8492 0.05830 0.05440 -0.1005 0.9753 0.0242
-16.250 -0.8371 0.05403 0.05003 -0.1067 0.9618 0.0243
-16.000 -0.8209 0.04985 0.04573 -0.1135 0.9509 0.0245
-15.750 -0.7992 0.04610 0.04187 -0.1206 0.9417 0.0246
-15.500 -0.7744 0.04239 0.03804 -0.1282 0.9352 0.0247
-15.250 -0.7493 0.03893 0.03446 -0.1356 0.9259 0.0248
-15.000 -0.7252 0.03610 0.03149 -0.1414 0.9135 0.0249
-14.500 -0.7162 0.03049 0.02560 -0.1463 0.8841 0.0251
-14.250 -0.7167 0.02802 0.02301 -0.1471 0.8729 0.0251
-14.000 -0.7175 0.02580 0.02068 -0.1474 0.8629 0.0253
-13.750 -0.7172 0.02388 0.01866 -0.1473 0.8548 0.0253
-13.500 -0.7167 0.02219 0.01689 -0.1467 0.8466 0.0255
-13.250 -0.7169 0.02080 0.01540 -0.1453 0.8389 0.0256
-13.000 -0.7145 0.01973 0.01427 -0.1434 0.8327 0.0257
-12.750 -0.7102 0.01891 0.01338 -0.1411 0.8260 0.0258
-12.500 -0.7054 0.01824 0.01263 -0.1385 0.8193 0.0260
-12.250 -0.6994 0.01763 0.01198 -0.1357 0.8138 0.0261
-12.000 -0.6921 0.01717 0.01146 -0.1327 0.8078 0.0262
-11.750 -0.6811 0.01677 0.01099 -0.1303 0.8023 0.0264
-11.500 -0.6655 0.01634 0.01052 -0.1287 0.7979 0.0266
-11.250 -0.6482 0.01593 0.01007 -0.1272 0.7932 0.0268
-11.000 -0.6297 0.01556 0.00965 -0.1259 0.7881 0.0270
-10.750 -0.6106 0.01520 0.00924 -0.1247 0.7831 0.0272
-10.500 -0.5903 0.01485 0.00884 -0.1236 0.7787 0.0274
-10.250 -0.5690 0.01451 0.00847 -0.1227 0.7738 0.0276
-10.000 -0.5473 0.01420 0.00811 -0.1218 0.7680 0.0279
-9.750 -0.5255 0.01391 0.00776 -0.1209 0.7619 0.0281
-9.500 -0.5023 0.01362 0.00743 -0.1202 0.7559 0.0283
-9.250 -0.4792 0.01335 0.00712 -0.1195 0.7489 0.0285
-9.000 -0.4565 0.01307 0.00678 -0.1186 0.7419 0.0288
-8.750 -0.4331 0.01277 0.00645 -0.1180 0.7347 0.0292
-8.500 -0.4097 0.01251 0.00614 -0.1172 0.7263 0.0296
-8.250 -0.3853 0.01226 0.00586 -0.1166 0.7197 0.0301
-8.000 -0.3606 0.01204 0.00561 -0.1161 0.7120 0.0305
-7.750 -0.3361 0.01185 0.00536 -0.1155 0.7037 0.0311
-7.500 -0.3110 0.01166 0.00514 -0.1150 0.6939 0.0317
-7.250 -0.2860 0.01151 0.00492 -0.1145 0.6856 0.0322
-7.000 -0.2603 0.01132 0.00470 -0.1140 0.6784 0.0328
-6.750 -0.2354 0.01115 0.00449 -0.1135 0.6700 0.0337
-6.500 -0.2097 0.01097 0.00429 -0.1131 0.6626 0.0347
-6.250 -0.1838 0.01083 0.00411 -0.1127 0.6552 0.0358
-6.000 -0.1580 0.01070 0.00394 -0.1122 0.6489 0.0371
-5.750 -0.1316 0.01052 0.00377 -0.1119 0.6433 0.0393
-5.000 -0.0528 0.01008 0.00332 -0.1110 0.6275 0.0508
-4.750 -0.0261 0.00992 0.00317 -0.1107 0.6229 0.0575
-4.500 0.0003 0.00976 0.00303 -0.1104 0.6180 0.0655
-4.250 0.0262 0.00960 0.00289 -0.1100 0.6131 0.0758
-4.000 0.0522 0.00937 0.00273 -0.1097 0.6090 0.0932
-3.750 0.0784 0.00914 0.00261 -0.1094 0.6043 0.1205
-3.500 0.1051 0.00904 0.00253 -0.1091 0.5985 0.1333
-3.250 0.1314 0.00896 0.00246 -0.1088 0.5930 0.1433
-3.000 0.1590 0.00888 0.00239 -0.1086 0.5887 0.1510
-2.750 0.1863 0.00879 0.00232 -0.1085 0.5836 0.1598
-2.500 0.2130 0.00870 0.00225 -0.1082 0.5780 0.1708
-2.250 0.2389 0.00858 0.00218 -0.1078 0.5727 0.1929
-2.000 0.2649 0.00834 0.00212 -0.1075 0.5674 0.2399
-1.750 0.2915 0.00827 0.00211 -0.1072 0.5607 0.2620
-1.500 0.3178 0.00825 0.00210 -0.1068 0.5541 0.2773
-1.250 0.3449 0.00822 0.00210 -0.1066 0.5466 0.2903
-1.000 0.3708 0.00826 0.00210 -0.1061 0.5372 0.2992
-0.750 0.3974 0.00827 0.00210 -0.1058 0.5273 0.3064
-0.500 0.4230 0.00833 0.00212 -0.1053 0.5165 0.3125
-0.250 0.4488 0.00839 0.00214 -0.1048 0.5047 0.3172
0.000 0.4740 0.00846 0.00217 -0.1042 0.4934 0.3228
0.250 0.4986 0.00854 0.00222 -0.1035 0.4821 0.3302
0.500 0.5237 0.00862 0.00226 -0.1029 0.4714 0.3372
0.750 0.5480 0.00870 0.00232 -0.1021 0.4618 0.3452
1.000 0.5728 0.00878 0.00238 -0.1015 0.4531 0.3525
1.500 0.6224 0.00892 0.00251 -0.1002 0.4400 0.3663
1.750 0.6462 0.00902 0.00259 -0.0993 0.4326 0.3745
2.000 0.6699 0.00911 0.00267 -0.0985 0.4259 0.3841
2.250 0.6940 0.00918 0.00275 -0.0977 0.4194 0.3956
2.500 0.7165 0.00928 0.00285 -0.0967 0.4130 0.4072
2.750 0.7394 0.00936 0.00294 -0.0956 0.4080 0.4191
3.000 0.7622 0.00939 0.00301 -0.0946 0.4044 0.4314
3.250 0.7843 0.00944 0.00309 -0.0934 0.4011 0.4439
3.500 0.8057 0.00951 0.00319 -0.0921 0.3975 0.4590
3.750 0.8262 0.00961 0.00331 -0.0907 0.3936 0.4710
4.000 0.8478 0.00971 0.00343 -0.0895 0.3902 0.4824
4.250 0.8707 0.00977 0.00355 -0.0885 0.3878 0.4961
4.500 0.8931 0.00985 0.00367 -0.0875 0.3850 0.5108
4.750 0.9147 0.00994 0.00382 -0.0863 0.3820 0.5310
5.000 0.9353 0.01003 0.00399 -0.0850 0.3788 0.5565
5.250 0.9552 0.01014 0.00418 -0.0835 0.3755 0.5887
5.500 0.9749 0.01026 0.00438 -0.0820 0.3724 0.6243
5.750 0.9966 0.01034 0.00455 -0.0809 0.3701 0.6514
6.000 1.0178 0.01045 0.00472 -0.0797 0.3662 0.6731
6.250 1.0371 0.01061 0.00492 -0.0782 0.3616 0.6938
6.500 1.0537 0.01082 0.00517 -0.0763 0.3558 0.7178
6.750 1.0714 0.01086 0.00539 -0.0745 0.3509 0.7688
7.000 1.1129 0.01089 0.00580 -0.0778 0.3375 0.9689
7.250 1.1375 0.01116 0.00606 -0.0775 0.3285 1.0000
7.500 1.1541 0.01152 0.00637 -0.0758 0.3207 1.0000
7.750 1.1722 0.01184 0.00667 -0.0743 0.3118 1.0000
8.000 1.1883 0.01226 0.00704 -0.0726 0.3033 1.0000
8.250 1.2031 0.01274 0.00747 -0.0708 0.2912 1.0000
8.500 1.2172 0.01327 0.00794 -0.0689 0.2788 1.0000
8.750 1.2300 0.01388 0.00849 -0.0669 0.2665 1.0000
9.000 1.2424 0.01455 0.00909 -0.0649 0.2545 1.0000
9.250 1.2555 0.01520 0.00969 -0.0632 0.2436 1.0000
9.500 1.2693 0.01585 0.01031 -0.0615 0.2342 1.0000
9.750 1.2814 0.01661 0.01102 -0.0597 0.2248 1.0000
10.000 1.2973 0.01721 0.01161 -0.0584 0.2184 1.0000
10.250 1.3104 0.01797 0.01234 -0.0569 0.2112 1.0000
10.500 1.3250 0.01867 0.01303 -0.0556 0.2046 1.0000
10.750 1.3381 0.01948 0.01383 -0.0542 0.1974 1.0000
11.000 1.3507 0.02035 0.01467 -0.0528 0.1894 1.0000
11.250 1.3614 0.02135 0.01563 -0.0513 0.1802 1.0000
11.500 1.3669 0.02270 0.01690 -0.0494 0.1645 1.0000
11.750 1.3713 0.02419 0.01830 -0.0475 0.1480 1.0000
12.000 1.3709 0.02606 0.02008 -0.0454 0.1293 1.0000
12.250 1.3711 0.02799 0.02192 -0.0436 0.1149 1.0000
12.500 1.3749 0.02974 0.02363 -0.0421 0.1046 1.0000
12.750 1.3825 0.03126 0.02514 -0.0410 0.0983 1.0000
13.000 1.3893 0.03289 0.02677 -0.0400 0.0934 1.0000
13.250 1.3976 0.03443 0.02832 -0.0391 0.0885 1.0000
13.500 1.4054 0.03606 0.02997 -0.0382 0.0854 1.0000
13.750 1.4118 0.03783 0.03173 -0.0374 0.0811 1.0000
14.000 1.4194 0.03952 0.03345 -0.0366 0.0781 1.0000
14.250 1.4252 0.04141 0.03535 -0.0359 0.0756 1.0000
14.500 1.4326 0.04317 0.03714 -0.0353 0.0731 1.0000
14.750 1.4391 0.04506 0.03907 -0.0347 0.0711 1.0000
15.000 1.4452 0.04696 0.04099 -0.0341 0.0692 1.0000
15.250 1.4487 0.04916 0.04322 -0.0335 0.0673 1.0000
15.500 1.4546 0.05115 0.04525 -0.0331 0.0659 1.0000
15.750 1.4594 0.05327 0.04741 -0.0326 0.0643 1.0000
16.000 1.4635 0.05547 0.04965 -0.0322 0.0629 1.0000
16.250 1.4663 0.05782 0.05204 -0.0318 0.0616 1.0000
16.500 1.4679 0.06033 0.05459 -0.0314 0.0604 1.0000
16.750 1.4703 0.06276 0.05706 -0.0311 0.0590 1.0000
17.000 1.4728 0.06524 0.05960 -0.0309 0.0583 1.0000
17.250 1.4759 0.06764 0.06205 -0.0307 0.0573 1.0000
17.500 1.4757 0.07043 0.06489 -0.0306 0.0560 1.0000
17.750 1.4757 0.07323 0.06774 -0.0305 0.0550 1.0000
18.000 1.4742 0.07622 0.07077 -0.0304 0.0538 1.0000
18.250 1.4721 0.07935 0.07395 -0.0305 0.0529 1.0000
18.500 1.4740 0.08199 0.07665 -0.0306 0.0524 1.0000
18.750 1.4735 0.08494 0.07966 -0.0308 0.0517 1.0000
19.000 1.4739 0.08780 0.08258 -0.0310 0.0508 1.0000
19.250 1.4725 0.09094 0.08578 -0.0313 0.0498 1.0000
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