GOE 570 AIRFOIL (goe570-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 570 AIRFOIL (goe570-il) Reynolds number: 1,000,000 Max Cl/Cd: 16.39 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe570-il-1000000-n5.txt Download as CSV file: xf-goe570-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 570 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 -0.0477 0.06231 0.05682 -0.2232 0.6877 0.0446
-19.500 -0.0515 0.05971 0.05418 -0.2242 0.6846 0.0451
-19.250 -0.0510 0.05765 0.05206 -0.2248 0.6817 0.0450
-19.000 -0.0535 0.05543 0.04976 -0.2254 0.6781 0.0448
-18.750 -0.0561 0.05306 0.04736 -0.2261 0.6757 0.0452
-18.500 -0.0553 0.05100 0.04528 -0.2267 0.6741 0.0455
-18.250 -0.0569 0.04887 0.04310 -0.2272 0.6714 0.0456
-18.000 -0.0588 0.04681 0.04100 -0.2275 0.6685 0.0456
-17.750 -0.0599 0.04490 0.03903 -0.2276 0.6646 0.0457
-17.500 -0.0586 0.04319 0.03728 -0.2277 0.6615 0.0461
-17.250 -0.0593 0.04149 0.03552 -0.2274 0.6583 0.0462
-17.000 -0.0584 0.03986 0.03384 -0.2272 0.6554 0.0464
-16.750 -0.0582 0.03820 0.03215 -0.2270 0.6532 0.0464
-16.500 -0.0581 0.03659 0.03050 -0.2267 0.6503 0.0466
-16.250 -0.0566 0.03514 0.02901 -0.2262 0.6468 0.0467
-16.000 -0.0522 0.03398 0.02782 -0.2255 0.6430 0.0472
-15.750 -0.0556 0.03252 0.02628 -0.2243 0.6388 0.0471
-15.500 -0.0572 0.03117 0.02488 -0.2230 0.6352 0.0471
-15.250 -0.0548 0.02996 0.02364 -0.2221 0.6327 0.0473
-15.000 -0.0520 0.02890 0.02255 -0.2208 0.6290 0.0476
-14.750 -0.0515 0.02791 0.02152 -0.2190 0.6247 0.0479
-14.500 -0.0542 0.02691 0.02046 -0.2168 0.6204 0.0480
-14.250 -0.0594 0.02589 0.01937 -0.2141 0.6158 0.0481
-14.000 -0.0604 0.02489 0.01834 -0.2120 0.6119 0.0480
-13.750 -0.0607 0.02404 0.01744 -0.2097 0.6075 0.0483
-13.500 -0.0633 0.02323 0.01658 -0.2069 0.6028 0.0482
-13.250 -0.0628 0.02267 0.01597 -0.2040 0.5978 0.0485
-13.000 -0.0652 0.02193 0.01518 -0.2010 0.5941 0.0485
-12.750 -0.0666 0.02131 0.01452 -0.1978 0.5896 0.0485
-12.500 -0.0675 0.02087 0.01403 -0.1943 0.5839 0.0487
-12.250 -0.0744 0.02046 0.01356 -0.1898 0.5785 0.0489
-12.000 -0.0807 0.02002 0.01307 -0.1852 0.5735 0.0489
-11.750 -0.0834 0.01964 0.01266 -0.1811 0.5696 0.0489
-11.500 -0.0871 0.01937 0.01234 -0.1766 0.5641 0.0491
-11.000 -0.0956 0.01887 0.01176 -0.1671 0.5555 0.0492
-10.750 -0.1008 0.01867 0.01153 -0.1620 0.5515 0.0493
-10.500 -0.1047 0.01851 0.01133 -0.1570 0.5470 0.0493
-10.250 -0.1123 0.01838 0.01114 -0.1513 0.5422 0.0494
-10.000 -0.1223 0.01823 0.01095 -0.1452 0.5380 0.0496
-9.750 -0.1274 0.01806 0.01077 -0.1399 0.5348 0.0498
-9.500 -0.1309 0.01796 0.01063 -0.1347 0.5305 0.0501
-9.250 -0.1375 0.01796 0.01059 -0.1289 0.5265 0.0500
-9.000 -0.1462 0.01791 0.01051 -0.1228 0.5226 0.0505
-8.750 -0.1503 0.01790 0.01047 -0.1174 0.5196 0.0506
-8.500 -0.1508 0.01787 0.01043 -0.1126 0.5168 0.0506
-8.250 -0.1530 0.01785 0.01039 -0.1075 0.5139 0.0509
-8.000 -0.1546 0.01790 0.01041 -0.1026 0.5105 0.0511
-7.750 -0.1547 0.01797 0.01045 -0.0978 0.5069 0.0512
-7.500 -0.1585 0.01810 0.01054 -0.0925 0.5027 0.0516
-7.250 -0.1548 0.01815 0.01057 -0.0885 0.5004 0.0518
-7.000 -0.1486 0.01817 0.01058 -0.0849 0.4976 0.0520
-6.750 -0.1433 0.01823 0.01062 -0.0811 0.4946 0.0522
-6.500 -0.1400 0.01835 0.01073 -0.0770 0.4917 0.0528
-6.250 -0.1356 0.01847 0.01081 -0.0732 0.4887 0.0529
-6.000 -0.1320 0.01862 0.01093 -0.0692 0.4853 0.0529
-5.750 -0.1289 0.01882 0.01111 -0.0652 0.4823 0.0533
-5.500 -0.1189 0.01891 0.01119 -0.0623 0.4801 0.0538
-5.250 -0.1088 0.01900 0.01127 -0.0595 0.4774 0.0541
-5.000 -0.0992 0.01913 0.01137 -0.0566 0.4744 0.0540
-4.750 -0.0920 0.01934 0.01156 -0.0534 0.4718 0.0545
-4.500 -0.0844 0.01958 0.01178 -0.0503 0.4686 0.0548
-4.250 -0.0756 0.01981 0.01198 -0.0474 0.4656 0.0551
-4.000 -0.0642 0.01997 0.01214 -0.0451 0.4633 0.0563
-3.750 -0.0505 0.02015 0.01231 -0.0431 0.4614 0.0563
-3.500 -0.0355 0.02030 0.01247 -0.0414 0.4594 0.0570
-3.250 -0.0202 0.02047 0.01264 -0.0397 0.4568 0.0578
-3.000 -0.0067 0.02073 0.01288 -0.0379 0.4535 0.0583
-2.750 0.0046 0.02109 0.01323 -0.0358 0.4506 0.0592
-2.500 0.0161 0.02147 0.01359 -0.0337 0.4471 0.0605
-2.250 0.0326 0.02173 0.01384 -0.0325 0.4449 0.0608
-2.000 0.0507 0.02194 0.01407 -0.0315 0.4430 0.0626
-1.750 0.0676 0.02223 0.01437 -0.0304 0.4410 0.0645
-1.500 0.0851 0.02250 0.01466 -0.0294 0.4387 0.0675
-1.250 0.1024 0.02278 0.01497 -0.0285 0.4360 0.0724
-1.000 0.1155 0.02326 0.01545 -0.0270 0.4322 0.0760
-0.750 0.1301 0.02370 0.01592 -0.0259 0.4301 0.0839
-0.500 0.1459 0.02411 0.01635 -0.0248 0.4274 0.0917
-0.250 0.1664 0.02437 0.01664 -0.0245 0.4257 0.0983
0.000 0.1862 0.02465 0.01696 -0.0241 0.4238 0.1050
0.250 0.2041 0.02503 0.01738 -0.0235 0.4216 0.1163
0.500 0.2222 0.02534 0.01790 -0.0231 0.4189 0.1618
0.750 0.2397 0.02578 0.01840 -0.0225 0.4168 0.1773
1.000 0.2533 0.02641 0.01900 -0.0214 0.4134 0.1824
1.250 0.2657 0.02710 0.01971 -0.0202 0.4104 0.1875
1.500 0.2843 0.02756 0.02019 -0.0197 0.4089 0.1925
1.750 0.3033 0.02800 0.02064 -0.0194 0.4072 0.1948
2.000 0.3220 0.02846 0.02110 -0.0190 0.4053 0.1975
2.250 0.3399 0.02895 0.02159 -0.0185 0.4032 0.1995
2.500 0.3566 0.02951 0.02216 -0.0180 0.4011 0.2038
2.750 0.3688 0.03032 0.02298 -0.0169 0.3983 0.2071
3.000 0.3808 0.03112 0.02377 -0.0159 0.3950 0.2104
3.250 0.3968 0.03173 0.02438 -0.0153 0.3931 0.2137
3.500 0.4162 0.03220 0.02487 -0.0152 0.3917 0.2149
3.750 0.4337 0.03280 0.02547 -0.0148 0.3898 0.2168
4.000 0.4493 0.03349 0.02619 -0.0143 0.3877 0.2228
4.250 0.4663 0.03410 0.02682 -0.0140 0.3859 0.2268
4.500 0.4824 0.03477 0.02751 -0.0136 0.3837 0.2329
5.000 0.5079 0.03649 0.02929 -0.0122 0.3786 0.2533
5.250 0.5236 0.03711 0.03040 -0.0124 0.3762 0.3914
5.500 0.5422 0.03762 0.03107 -0.0124 0.3751 0.4329
5.750 0.5596 0.03825 0.03176 -0.0123 0.3731 0.4480
6.000 0.5766 0.03890 0.03245 -0.0121 0.3714 0.4603
6.250 0.5920 0.03964 0.03324 -0.0118 0.3694 0.4765
6.500 0.6027 0.04066 0.03434 -0.0110 0.3672 0.4952
6.750 0.6150 0.04161 0.03531 -0.0104 0.3651 0.5068
7.000 0.6271 0.04256 0.03630 -0.0098 0.3627 0.5211
7.250 0.6387 0.04352 0.03733 -0.0092 0.3603 0.5429
7.500 0.6516 0.04441 0.03833 -0.0087 0.3589 0.5690
7.750 0.6661 0.04520 0.03921 -0.0084 0.3578 0.5933
8.000 0.6777 0.04576 0.04010 -0.0074 0.3561 0.6759
8.500 0.8220 0.05016 0.04548 -0.0320 0.3520 0.9568
8.750 0.8348 0.05142 0.04673 -0.0318 0.3495 0.9609
9.000 0.8390 0.05308 0.04838 -0.0307 0.3469 0.9641
9.250 0.8444 0.05447 0.04976 -0.0294 0.3445 0.9662
9.500 0.8505 0.05535 0.05064 -0.0275 0.3431 0.9693
9.750 0.8461 0.05596 0.05127 -0.0231 0.3420 0.9717
10.000 0.8679 0.05740 0.05272 -0.0251 0.3404 0.9725
10.250 0.8835 0.05885 0.05418 -0.0260 0.3385 0.9730
10.500 0.9030 0.06019 0.05553 -0.0275 0.3367 0.9737
10.750 0.9191 0.06152 0.05685 -0.0284 0.3348 0.9743
11.000 0.9431 0.06334 0.05868 -0.0314 0.3327 0.9758
11.250 0.9469 0.06538 0.06071 -0.0309 0.3303 0.9763
11.500 0.9640 0.06708 0.06241 -0.0325 0.3279 0.9774
11.750 0.9834 0.06831 0.06366 -0.0339 0.3271 0.9784
12.000 1.0061 0.06974 0.06511 -0.0361 0.3260 0.9800
12.250 1.0215 0.07143 0.06682 -0.0374 0.3242 0.9812
12.500 1.0330 0.07328 0.06871 -0.0381 0.3221 0.9824
12.750 1.0523 0.07496 0.07040 -0.0401 0.3206 0.9843
13.000 1.0652 0.07660 0.07204 -0.0408 0.3188 0.9856
13.250 1.0737 0.07870 0.07414 -0.0411 0.3163 0.9875
13.500 1.0714 0.08096 0.07640 -0.0398 0.3137 0.9882
13.750 1.0797 0.08218 0.07764 -0.0393 0.3124 0.9884
14.000 1.0852 0.08340 0.07888 -0.0380 0.3113 0.9889
14.250 1.1048 0.08498 0.08049 -0.0402 0.3102 0.9896
14.500 1.1211 0.08674 0.08229 -0.0421 0.3087 0.9902
14.750 1.1117 0.08814 0.08371 -0.0385 0.3072 0.9895
15.000 1.1320 0.09006 0.08564 -0.0414 0.3054 0.9903
15.250 1.1435 0.09176 0.08735 -0.0423 0.3034 0.9907
15.500 1.1497 0.09334 0.08894 -0.0421 0.3017 0.9907
15.750 1.1492 0.09554 0.09114 -0.0414 0.2994 0.9908
16.000 1.1511 0.09709 0.09270 -0.0404 0.2970 0.9906
16.250 1.1637 0.09853 0.09418 -0.0412 0.2962 0.9909
16.500 1.1704 0.10006 0.09575 -0.0411 0.2948 0.9910
16.750 1.1740 0.10190 0.09762 -0.0409 0.2926 0.9910
17.000 1.1762 0.10386 0.09961 -0.0405 0.2912 0.9911
17.250 1.1808 0.10557 0.10133 -0.0404 0.2889 0.9911
17.500 1.1837 0.10744 0.10318 -0.0401 0.2860 0.9912
17.750 1.1906 0.10891 0.10463 -0.0402 0.2836 0.9912
18.000 1.1881 0.11136 0.10715 -0.0397 0.2819 0.9913
18.250 1.1924 0.11311 0.10894 -0.0396 0.2803 0.9913
18.500 1.1992 0.11461 0.11047 -0.0397 0.2789 0.9914
18.750 1.2068 0.11601 0.11190 -0.0399 0.2777 0.9914
19.000 1.1976 0.11911 0.11501 -0.0392 0.2731 0.9915
19.250 1.2033 0.12068 0.11657 -0.0393 0.2714 0.9915
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