GOE 628 AIRFOIL (goe628-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 628 AIRFOIL (goe628-il) Reynolds number: 1,000,000 Max Cl/Cd: 107.79 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe628-il-1000000-n5.txt Download as CSV file: xf-goe628-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 628 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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7469 0.11104 0.10838 -0.0628 1.0000 0.0206
-18.750 -0.7891 0.10073 0.09794 -0.0690 1.0000 0.0214
-18.500 -0.8127 0.09373 0.09085 -0.0732 1.0000 0.0218
-18.250 -0.8380 0.08668 0.08373 -0.0774 1.0000 0.0228
-18.000 -0.8632 0.07987 0.07685 -0.0814 1.0000 0.0240
-17.750 -0.8817 0.07424 0.07116 -0.0847 1.0000 0.0249
-17.500 -0.8974 0.06920 0.06606 -0.0875 1.0000 0.0258
-17.250 -0.9154 0.06407 0.06088 -0.0903 1.0000 0.0265
-17.000 -0.9354 0.05903 0.05577 -0.0929 1.0000 0.0271
-16.750 -0.9600 0.05393 0.05061 -0.0954 1.0000 0.0277
-16.500 -0.9891 0.04873 0.04533 -0.0976 1.0000 0.0283
-16.000 -1.0373 0.03528 0.03165 -0.1106 0.9911 0.0288
-15.750 -1.0459 0.02589 0.02197 -0.1252 0.9799 0.0294
-15.500 -1.0269 0.02429 0.02032 -0.1269 0.9728 0.0305
-15.250 -0.9980 0.02315 0.01911 -0.1291 0.9689 0.0316
-15.000 -0.9685 0.02212 0.01801 -0.1313 0.9648 0.0326
-14.750 -0.9383 0.02118 0.01698 -0.1333 0.9592 0.0332
-14.500 -0.9044 0.02042 0.01619 -0.1356 0.9542 0.0340
-14.250 -0.8725 0.01980 0.01553 -0.1372 0.9470 0.0347
-14.000 -0.8412 0.01925 0.01492 -0.1385 0.9384 0.0354
-13.750 -0.8143 0.01875 0.01434 -0.1390 0.9280 0.0360
-13.500 -0.7885 0.01830 0.01380 -0.1390 0.9169 0.0367
-13.250 -0.7665 0.01787 0.01328 -0.1384 0.9041 0.0371
-13.000 -0.7445 0.01747 0.01278 -0.1376 0.8925 0.0374
-12.750 -0.7242 0.01700 0.01223 -0.1366 0.8789 0.0378
-12.500 -0.7035 0.01660 0.01175 -0.1356 0.8639 0.0382
-12.250 -0.6813 0.01630 0.01138 -0.1346 0.8480 0.0386
-12.000 -0.6587 0.01605 0.01105 -0.1337 0.8300 0.0391
-11.750 -0.6363 0.01584 0.01073 -0.1326 0.8092 0.0396
-11.500 -0.6137 0.01566 0.01044 -0.1316 0.7884 0.0401
-11.000 -0.5691 0.01515 0.00971 -0.1295 0.7530 0.0409
-10.750 -0.5454 0.01490 0.00937 -0.1287 0.7406 0.0412
-10.250 -0.4966 0.01445 0.00876 -0.1273 0.7205 0.0419
-10.000 -0.4725 0.01420 0.00842 -0.1266 0.7115 0.0423
-9.750 -0.4485 0.01383 0.00801 -0.1259 0.7049 0.0429
-9.500 -0.4233 0.01358 0.00773 -0.1253 0.6979 0.0434
-9.250 -0.3985 0.01333 0.00742 -0.1246 0.6908 0.0437
-9.000 -0.3727 0.01308 0.00713 -0.1241 0.6850 0.0440
-8.750 -0.3470 0.01284 0.00685 -0.1236 0.6790 0.0443
-8.500 -0.3215 0.01261 0.00656 -0.1230 0.6728 0.0446
-8.250 -0.2955 0.01237 0.00627 -0.1225 0.6672 0.0449
-8.000 -0.2693 0.01214 0.00600 -0.1220 0.6614 0.0452
-7.750 -0.2432 0.01193 0.00574 -0.1215 0.6553 0.0455
-7.500 -0.2171 0.01173 0.00549 -0.1210 0.6490 0.0458
-7.250 -0.1905 0.01153 0.00525 -0.1206 0.6412 0.0461
-7.000 -0.1646 0.01138 0.00502 -0.1200 0.6320 0.0464
-6.750 -0.1378 0.01122 0.00480 -0.1196 0.6228 0.0467
-6.250 -0.0847 0.01094 0.00441 -0.1186 0.6043 0.0471
-6.000 -0.0582 0.01078 0.00419 -0.1182 0.5970 0.0475
-5.750 -0.0317 0.01058 0.00395 -0.1177 0.5909 0.0480
-5.500 -0.0047 0.01042 0.00376 -0.1173 0.5836 0.0485
-5.250 0.0218 0.01030 0.00359 -0.1168 0.5757 0.0490
-5.000 0.0491 0.01018 0.00344 -0.1165 0.5688 0.0496
-4.750 0.0763 0.01008 0.00331 -0.1161 0.5617 0.0502
-4.500 0.1033 0.01000 0.00318 -0.1157 0.5549 0.0508
-4.250 0.1307 0.00991 0.00306 -0.1154 0.5473 0.0513
-4.000 0.1574 0.00986 0.00295 -0.1149 0.5387 0.0519
-3.750 0.1848 0.00979 0.00285 -0.1146 0.5309 0.0524
-3.500 0.2119 0.00974 0.00276 -0.1142 0.5230 0.0529
-3.250 0.2390 0.00967 0.00266 -0.1138 0.5160 0.0538
-3.000 0.2661 0.00960 0.00256 -0.1134 0.5082 0.0549
-2.750 0.2928 0.00957 0.00249 -0.1129 0.4999 0.0560
-2.500 0.3199 0.00953 0.00242 -0.1126 0.4905 0.0573
-2.250 0.3465 0.00954 0.00238 -0.1121 0.4809 0.0585
-2.000 0.3734 0.00952 0.00233 -0.1117 0.4715 0.0605
-1.750 0.3998 0.00950 0.00229 -0.1112 0.4627 0.0647
-1.500 0.4255 0.00931 0.00220 -0.1107 0.4533 0.1009
-1.250 0.4511 0.00922 0.00216 -0.1101 0.4441 0.1292
-1.000 0.4766 0.00913 0.00214 -0.1096 0.4331 0.1599
-0.750 0.5021 0.00911 0.00215 -0.1090 0.4212 0.1871
-0.500 0.5275 0.00915 0.00219 -0.1083 0.4094 0.2049
-0.250 0.5534 0.00920 0.00223 -0.1078 0.3982 0.2179
0.000 0.5791 0.00927 0.00229 -0.1072 0.3885 0.2304
0.250 0.6046 0.00934 0.00235 -0.1066 0.3780 0.2427
0.500 0.6305 0.00942 0.00241 -0.1061 0.3695 0.2517
0.750 0.6556 0.00951 0.00249 -0.1054 0.3601 0.2646
1.000 0.6812 0.00959 0.00257 -0.1048 0.3525 0.2763
1.250 0.7063 0.00970 0.00266 -0.1042 0.3439 0.2867
1.500 0.7315 0.00979 0.00275 -0.1035 0.3373 0.2951
1.750 0.7570 0.00988 0.00283 -0.1029 0.3317 0.3029
2.000 0.7821 0.00999 0.00292 -0.1023 0.3262 0.3084
2.250 0.8069 0.01009 0.00303 -0.1016 0.3214 0.3165
2.500 0.8323 0.01017 0.00312 -0.1010 0.3176 0.3244
2.750 0.8571 0.01026 0.00322 -0.1003 0.3131 0.3337
3.000 0.8810 0.01039 0.00334 -0.0994 0.3081 0.3408
3.250 0.9052 0.01052 0.00345 -0.0986 0.3041 0.3469
3.500 0.9298 0.01059 0.00356 -0.0979 0.3014 0.3540
3.750 0.9540 0.01069 0.00367 -0.0971 0.2985 0.3609
4.000 0.9777 0.01081 0.00379 -0.0962 0.2953 0.3666
4.250 1.0002 0.01093 0.00392 -0.0951 0.2921 0.3743
4.500 1.0210 0.01107 0.00406 -0.0937 0.2885 0.3825
4.750 1.0426 0.01116 0.00418 -0.0924 0.2860 0.3901
5.000 1.0643 0.01125 0.00431 -0.0912 0.2836 0.3991
5.250 1.0858 0.01137 0.00445 -0.0899 0.2812 0.4071
5.500 1.1066 0.01151 0.00462 -0.0886 0.2787 0.4185
5.750 1.1270 0.01167 0.00480 -0.0871 0.2761 0.4300
6.000 1.1470 0.01184 0.00500 -0.0857 0.2733 0.4443
6.250 1.1663 0.01202 0.00523 -0.0841 0.2704 0.4610
6.750 1.2074 0.01223 0.00563 -0.0815 0.2666 0.5262
7.250 1.2892 0.01196 0.00633 -0.0878 0.2610 1.0000
7.500 1.3089 0.01221 0.00658 -0.0864 0.2585 1.0000
7.750 1.3275 0.01251 0.00686 -0.0849 0.2549 1.0000
8.000 1.3481 0.01275 0.00710 -0.0838 0.2527 1.0000
8.250 1.3688 0.01299 0.00736 -0.0827 0.2501 1.0000
8.500 1.3886 0.01328 0.00764 -0.0815 0.2464 1.0000
8.750 1.4072 0.01362 0.00797 -0.0801 0.2427 1.0000
9.000 1.4252 0.01400 0.00834 -0.0788 0.2394 1.0000
9.250 1.4447 0.01433 0.00869 -0.0777 0.2370 1.0000
9.500 1.4645 0.01465 0.00903 -0.0766 0.2350 1.0000
9.750 1.4840 0.01500 0.00940 -0.0756 0.2329 1.0000
10.000 1.5028 0.01539 0.00981 -0.0745 0.2304 1.0000
10.250 1.5208 0.01584 0.01027 -0.0734 0.2279 1.0000
10.500 1.5381 0.01634 0.01078 -0.0722 0.2252 1.0000
10.750 1.5548 0.01689 0.01133 -0.0710 0.2224 1.0000
11.000 1.5737 0.01733 0.01181 -0.0701 0.2202 1.0000
11.250 1.5915 0.01785 0.01236 -0.0692 0.2180 1.0000
11.500 1.6085 0.01842 0.01296 -0.0682 0.2149 1.0000
11.750 1.6239 0.01910 0.01365 -0.0671 0.2119 1.0000
12.000 1.6384 0.01986 0.01442 -0.0659 0.2088 1.0000
12.250 1.6541 0.02057 0.01515 -0.0650 0.2055 1.0000
12.500 1.6690 0.02133 0.01594 -0.0640 0.2011 1.0000
12.750 1.6791 0.02243 0.01702 -0.0627 0.1949 1.0000
13.000 1.6919 0.02339 0.01800 -0.0616 0.1902 1.0000
13.250 1.7025 0.02453 0.01914 -0.0605 0.1841 1.0000
13.500 1.7102 0.02590 0.02050 -0.0593 0.1775 1.0000
13.750 1.7177 0.02734 0.02194 -0.0581 0.1702 1.0000
14.000 1.7241 0.02891 0.02351 -0.0570 0.1647 1.0000
14.250 1.7296 0.03058 0.02518 -0.0559 0.1575 1.0000
14.500 1.7339 0.03240 0.02701 -0.0549 0.1521 1.0000
14.750 1.7374 0.03431 0.02893 -0.0539 0.1452 1.0000
15.000 1.7362 0.03669 0.03130 -0.0528 0.1374 1.0000
15.250 1.7370 0.03894 0.03356 -0.0519 0.1319 1.0000
15.500 1.7354 0.04147 0.03610 -0.0510 0.1261 1.0000
15.750 1.7330 0.04413 0.03878 -0.0503 0.1203 1.0000
16.000 1.7317 0.04673 0.04141 -0.0496 0.1166 1.0000
16.250 1.7314 0.04927 0.04399 -0.0491 0.1125 1.0000
16.500 1.7293 0.05208 0.04685 -0.0486 0.1094 1.0000
16.750 1.7227 0.05541 0.05022 -0.0482 0.1051 1.0000
17.000 1.7222 0.05812 0.05299 -0.0480 0.1029 1.0000
17.250 1.7178 0.06131 0.05622 -0.0478 0.0997 1.0000
17.500 1.7058 0.06542 0.06036 -0.0477 0.0952 1.0000
17.750 1.7036 0.06848 0.06350 -0.0477 0.0939 1.0000
18.000 1.6947 0.07233 0.06741 -0.0478 0.0903 1.0000
18.250 1.6782 0.07717 0.07228 -0.0481 0.0860 1.0000
18.500 1.6704 0.08103 0.07622 -0.0484 0.0833 1.0000
18.750 1.6603 0.08518 0.08043 -0.0488 0.0805 1.0000
19.000 1.6446 0.09010 0.08540 -0.0494 0.0775 1.0000
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