GOE 256 (JUNKERS E) AIRFOIL (goe256-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 256 (JUNKERS E) AIRFOIL (goe256-il) Reynolds number: 1,000,000 Max Cl/Cd: 103.55 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe256-il-1000000-n5.txt Download as CSV file: xf-goe256-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 256 (JUNKERS E) 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
------ -------- --------- --------- -------- -------- --------
-16.750 -1.0549 0.03624 0.03286 -0.1196 0.9960 0.0252
-16.500 -1.0529 0.03286 0.02933 -0.1229 0.9851 0.0253
-16.250 -1.0458 0.03063 0.02698 -0.1242 0.9719 0.0255
-16.000 -1.0383 0.02897 0.02520 -0.1241 0.9555 0.0256
-15.750 -1.0325 0.02769 0.02379 -0.1227 0.9383 0.0258
-15.500 -1.0256 0.02660 0.02257 -0.1210 0.9240 0.0259
-15.250 -1.0169 0.02560 0.02145 -0.1193 0.9126 0.0261
-15.000 -1.0070 0.02468 0.02041 -0.1175 0.9035 0.0262
-14.750 -0.9959 0.02386 0.01947 -0.1157 0.8951 0.0263
-14.500 -0.9834 0.02312 0.01863 -0.1139 0.8880 0.0265
-14.250 -0.9672 0.02239 0.01779 -0.1127 0.8812 0.0267
-14.000 -0.9501 0.02170 0.01699 -0.1115 0.8744 0.0268
-13.750 -0.9318 0.02104 0.01624 -0.1105 0.8685 0.0270
-13.500 -0.9125 0.02041 0.01552 -0.1095 0.8619 0.0272
-13.250 -0.8927 0.01983 0.01483 -0.1086 0.8554 0.0273
-13.000 -0.8718 0.01927 0.01418 -0.1078 0.8495 0.0275
-12.750 -0.8505 0.01874 0.01356 -0.1070 0.8424 0.0276
-12.500 -0.8287 0.01825 0.01297 -0.1063 0.8357 0.0278
-12.250 -0.8061 0.01778 0.01241 -0.1056 0.8286 0.0279
-12.000 -0.7840 0.01729 0.01183 -0.1049 0.8214 0.0281
-11.750 -0.7621 0.01672 0.01119 -0.1041 0.8150 0.0284
-11.500 -0.7392 0.01624 0.01064 -0.1035 0.8079 0.0287
-11.250 -0.7157 0.01584 0.01017 -0.1029 0.8015 0.0290
-11.000 -0.6912 0.01547 0.00976 -0.1025 0.7953 0.0293
-10.750 -0.6667 0.01513 0.00935 -0.1020 0.7889 0.0296
-10.500 -0.6419 0.01479 0.00895 -0.1016 0.7833 0.0299
-10.250 -0.6167 0.01446 0.00857 -0.1012 0.7779 0.0302
-10.000 -0.5915 0.01415 0.00820 -0.1008 0.7723 0.0305
-9.750 -0.5662 0.01386 0.00784 -0.1004 0.7672 0.0308
-9.500 -0.5404 0.01357 0.00749 -0.1001 0.7625 0.0311
-9.250 -0.5145 0.01329 0.00716 -0.0998 0.7579 0.0314
-9.000 -0.4885 0.01303 0.00684 -0.0995 0.7538 0.0317
-8.750 -0.4623 0.01279 0.00654 -0.0992 0.7500 0.0320
-8.500 -0.4360 0.01250 0.00622 -0.0990 0.7469 0.0323
-8.250 -0.4098 0.01221 0.00590 -0.0987 0.7434 0.0328
-8.000 -0.3833 0.01197 0.00564 -0.0985 0.7398 0.0334
-7.750 -0.3567 0.01176 0.00539 -0.0983 0.7363 0.0339
-7.500 -0.3300 0.01157 0.00517 -0.0980 0.7329 0.0344
-7.250 -0.3028 0.01137 0.00495 -0.0979 0.7290 0.0350
-7.000 -0.2759 0.01119 0.00473 -0.0977 0.7228 0.0357
-6.500 -0.2222 0.01087 0.00432 -0.0973 0.7108 0.0370
-6.250 -0.1952 0.01068 0.00412 -0.0971 0.7061 0.0379
-6.000 -0.1680 0.01053 0.00395 -0.0970 0.7020 0.0388
-5.750 -0.1408 0.01040 0.00379 -0.0968 0.6983 0.0397
-5.500 -0.1131 0.01026 0.00364 -0.0968 0.6954 0.0407
-5.250 -0.0852 0.01012 0.00349 -0.0967 0.6921 0.0416
-5.000 -0.0577 0.00997 0.00334 -0.0967 0.6884 0.0429
-4.750 -0.0302 0.00985 0.00322 -0.0966 0.6845 0.0443
-4.500 -0.0028 0.00976 0.00310 -0.0965 0.6805 0.0457
-4.250 0.0252 0.00966 0.00299 -0.0965 0.6771 0.0470
-4.000 0.0531 0.00954 0.00288 -0.0964 0.6730 0.0487
-3.750 0.0808 0.00944 0.00279 -0.0964 0.6686 0.0505
-3.500 0.1083 0.00937 0.00270 -0.0963 0.6640 0.0521
-3.250 0.1362 0.00930 0.00261 -0.0963 0.6595 0.0534
-3.000 0.1640 0.00920 0.00252 -0.0962 0.6542 0.0553
-2.750 0.1915 0.00913 0.00246 -0.0961 0.6485 0.0572
-2.500 0.2191 0.00908 0.00239 -0.0960 0.6429 0.0589
-2.250 0.2469 0.00904 0.00233 -0.0960 0.6353 0.0605
-2.000 0.2737 0.00899 0.00226 -0.0958 0.6265 0.0627
-1.750 0.3008 0.00895 0.00221 -0.0956 0.6155 0.0649
-1.500 0.3275 0.00894 0.00217 -0.0954 0.6035 0.0669
-1.250 0.3535 0.00897 0.00214 -0.0950 0.5877 0.0686
-1.000 0.3785 0.00902 0.00212 -0.0944 0.5678 0.0712
-0.750 0.4027 0.00912 0.00214 -0.0937 0.5460 0.0738
-0.500 0.4271 0.00923 0.00216 -0.0930 0.5259 0.0761
-0.250 0.4519 0.00934 0.00219 -0.0924 0.5088 0.0781
0.000 0.4769 0.00941 0.00222 -0.0919 0.4947 0.0816
0.250 0.5025 0.00946 0.00225 -0.0915 0.4828 0.0852
0.500 0.5278 0.00953 0.00228 -0.0910 0.4720 0.0890
0.750 0.5531 0.00958 0.00233 -0.0906 0.4614 0.0973
1.000 0.5784 0.00961 0.00237 -0.0901 0.4522 0.1122
1.250 0.6028 0.00962 0.00243 -0.0895 0.4423 0.1438
1.500 0.6264 0.00941 0.00249 -0.0889 0.4345 0.2501
1.750 0.6501 0.00931 0.00257 -0.0883 0.4264 0.3299
2.250 0.6976 0.00903 0.00274 -0.0870 0.4142 0.5063
2.500 0.7179 0.00870 0.00285 -0.0857 0.4082 0.6691
2.750 0.7293 0.00824 0.00313 -0.0819 0.4038 0.9233
3.000 0.7520 0.00837 0.00327 -0.0807 0.3988 0.9441
3.250 0.7744 0.00853 0.00341 -0.0794 0.3935 0.9583
3.500 0.7962 0.00871 0.00356 -0.0781 0.3883 0.9685
3.750 0.8260 0.00887 0.00371 -0.0786 0.3837 0.9758
4.000 0.8510 0.00902 0.00383 -0.0781 0.3785 0.9810
4.500 0.9359 0.00957 0.00428 -0.0849 0.3621 0.9878
4.750 0.9656 0.00982 0.00446 -0.0856 0.3536 0.9900
5.000 0.9906 0.00996 0.00458 -0.0852 0.3488 0.9914
5.250 1.0141 0.01012 0.00473 -0.0846 0.3436 0.9929
5.500 1.0405 0.01032 0.00489 -0.0846 0.3386 0.9937
5.750 1.0678 0.01047 0.00504 -0.0848 0.3348 0.9946
6.000 1.0942 0.01064 0.00520 -0.0849 0.3300 0.9958
6.250 1.1187 0.01086 0.00540 -0.0846 0.3244 0.9970
6.500 1.1430 0.01108 0.00560 -0.0843 0.3192 0.9984
6.750 1.1680 0.01128 0.00579 -0.0841 0.3147 0.9996
7.000 1.1813 0.01145 0.00597 -0.0814 0.3109 1.0000
7.250 1.1893 0.01164 0.00616 -0.0777 0.3073 1.0000
7.500 1.2004 0.01186 0.00637 -0.0747 0.3034 1.0000
7.750 1.2169 0.01207 0.00659 -0.0728 0.2993 1.0000
8.000 1.2346 0.01234 0.00686 -0.0712 0.2944 1.0000
8.250 1.2519 0.01270 0.00719 -0.0697 0.2887 1.0000
8.500 1.2717 0.01300 0.00750 -0.0686 0.2830 1.0000
8.750 1.2895 0.01340 0.00788 -0.0673 0.2750 1.0000
9.000 1.3085 0.01379 0.00826 -0.0662 0.2691 1.0000
9.250 1.3258 0.01428 0.00872 -0.0649 0.2593 1.0000
9.500 1.3417 0.01485 0.00924 -0.0635 0.2465 1.0000
9.750 1.3531 0.01568 0.00996 -0.0615 0.2269 1.0000
10.250 1.3618 0.01823 0.01217 -0.0561 0.1700 1.0000
10.500 1.3706 0.01932 0.01318 -0.0541 0.1548 1.0000
10.750 1.3827 0.02025 0.01408 -0.0525 0.1451 1.0000
11.000 1.3959 0.02114 0.01494 -0.0512 0.1380 1.0000
11.250 1.4081 0.02209 0.01587 -0.0498 0.1306 1.0000
11.500 1.4216 0.02299 0.01678 -0.0486 0.1252 1.0000
11.750 1.4353 0.02389 0.01768 -0.0475 0.1206 1.0000
12.000 1.4472 0.02493 0.01871 -0.0463 0.1159 1.0000
12.250 1.4610 0.02585 0.01965 -0.0453 0.1124 1.0000
12.500 1.4725 0.02695 0.02076 -0.0442 0.1076 1.0000
12.750 1.4825 0.02820 0.02200 -0.0429 0.1026 1.0000
13.000 1.4953 0.02926 0.02309 -0.0420 0.0994 1.0000
13.250 1.5056 0.03053 0.02437 -0.0410 0.0953 1.0000
13.500 1.5146 0.03192 0.02575 -0.0399 0.0910 1.0000
13.750 1.5243 0.03328 0.02715 -0.0389 0.0867 1.0000
14.000 1.5296 0.03504 0.02888 -0.0377 0.0803 1.0000
14.250 1.5317 0.03710 0.03091 -0.0363 0.0713 1.0000
14.500 1.5248 0.03999 0.03372 -0.0346 0.0561 1.0000
14.750 1.5038 0.04431 0.03796 -0.0323 0.0360 1.0000
15.000 1.4978 0.04741 0.04106 -0.0310 0.0292 1.0000
15.250 1.4971 0.05004 0.04373 -0.0302 0.0258 1.0000
15.500 1.4973 0.05268 0.04642 -0.0295 0.0236 1.0000
15.750 1.4978 0.05536 0.04914 -0.0290 0.0218 1.0000
16.000 1.4982 0.05810 0.05194 -0.0285 0.0205 1.0000
16.250 1.4992 0.06081 0.05470 -0.0282 0.0194 1.0000
16.500 1.4985 0.06375 0.05770 -0.0279 0.0183 1.0000
16.750 1.4974 0.06681 0.06082 -0.0277 0.0175 1.0000
17.000 1.4968 0.06987 0.06395 -0.0277 0.0168 1.0000
17.250 1.4951 0.07308 0.06723 -0.0277 0.0161 1.0000
17.500 1.4924 0.07644 0.07065 -0.0278 0.0155 1.0000
17.750 1.4891 0.07990 0.07417 -0.0280 0.0149 1.0000
18.000 1.4867 0.08328 0.07763 -0.0283 0.0145 1.0000
18.250 1.4837 0.08679 0.08120 -0.0286 0.0142 1.0000
18.500 1.4804 0.09036 0.08485 -0.0291 0.0138 1.0000
18.750 1.4771 0.09390 0.08847 -0.0295 0.0135 1.0000
19.000 1.4730 0.09760 0.09223 -0.0301 0.0132 1.0000
19.250 1.4681 0.10144 0.09614 -0.0308 0.0129 1.0000
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