GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 435 AIRFOIL (goe435-il) Reynolds number: 500,000 Max Cl/Cd: 75.77 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe435-il-500000.txt Download as CSV file: xf-goe435-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 435 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8245 0.10577 0.10112 -0.0660 1.0000 0.0716
-19.500 -0.8149 0.10373 0.09907 -0.0672 1.0000 0.0719
-19.250 -0.8051 0.10171 0.09704 -0.0683 1.0000 0.0721
-19.000 -0.7951 0.09972 0.09504 -0.0694 1.0000 0.0724
-18.750 -0.7846 0.09780 0.09311 -0.0704 1.0000 0.0726
-18.500 -0.7740 0.09590 0.09120 -0.0714 1.0000 0.0728
-18.250 -0.7636 0.09397 0.08926 -0.0724 1.0000 0.0730
-18.000 -0.7533 0.09202 0.08730 -0.0735 1.0000 0.0732
-17.750 -0.7432 0.09002 0.08529 -0.0746 1.0000 0.0734
-17.500 -0.7328 0.08805 0.08332 -0.0757 1.0000 0.0736
-17.250 -0.7224 0.08611 0.08137 -0.0768 1.0000 0.0738
-17.000 -0.7122 0.08412 0.07939 -0.0779 1.0000 0.0740
-16.750 -0.6975 0.08193 0.07716 -0.0804 0.9761 0.0743
-16.500 -0.6870 0.07973 0.07491 -0.0818 0.9526 0.0745
-16.250 -0.6829 0.07779 0.07289 -0.0816 0.9262 0.0747
-16.000 -0.6786 0.07591 0.07091 -0.0814 0.9010 0.0749
-15.750 -0.6735 0.07391 0.06880 -0.0815 0.8785 0.0751
-15.500 -0.6682 0.07176 0.06651 -0.0820 0.8601 0.0753
-15.250 -0.6626 0.06956 0.06419 -0.0826 0.8442 0.0755
-15.000 -0.6555 0.06742 0.06196 -0.0834 0.8315 0.0757
-14.750 -0.6491 0.06532 0.05975 -0.0842 0.8205 0.0760
-14.500 -0.6438 0.06297 0.05738 -0.0852 0.8128 0.0764
-14.250 -0.6400 0.06050 0.05485 -0.0863 0.8050 0.0768
-14.000 -0.6375 0.05791 0.05218 -0.0874 0.7974 0.0772
-13.750 -0.6368 0.05502 0.04923 -0.0889 0.7913 0.0776
-13.500 -0.6350 0.05230 0.04646 -0.0902 0.7857 0.0780
-13.250 -0.6351 0.04938 0.04348 -0.0917 0.7803 0.0784
-13.000 -0.6333 0.04678 0.04079 -0.0929 0.7750 0.0789
-12.750 -0.6330 0.04406 0.03798 -0.0943 0.7694 0.0793
-12.500 -0.6308 0.04156 0.03544 -0.0956 0.7657 0.0798
-12.250 -0.6291 0.03899 0.03282 -0.0970 0.7613 0.0803
-12.000 -0.6258 0.03659 0.03035 -0.0983 0.7566 0.0808
-11.750 -0.6212 0.03430 0.02798 -0.0995 0.7519 0.0814
-11.500 -0.6152 0.03209 0.02568 -0.1008 0.7472 0.0820
-11.250 -0.6072 0.03002 0.02352 -0.1022 0.7426 0.0828
-11.000 -0.6023 0.02748 0.02095 -0.1041 0.7393 0.0841
-10.750 -0.5948 0.02516 0.01860 -0.1059 0.7353 0.0856
-10.500 -0.5881 0.02319 0.01657 -0.1073 0.7310 0.0873
-10.000 -0.5585 0.01854 0.01206 -0.1148 0.7219 0.1255
-9.750 -0.5293 0.01831 0.01181 -0.1158 0.7168 0.1389
-9.500 -0.4995 0.01815 0.01163 -0.1164 0.7136 0.1446
-9.250 -0.4705 0.01787 0.01136 -0.1173 0.7095 0.1482
-9.000 -0.4405 0.01774 0.01121 -0.1180 0.7050 0.1520
-8.750 -0.4105 0.01764 0.01104 -0.1187 0.7002 0.1548
-8.500 -0.3802 0.01764 0.01091 -0.1194 0.6949 0.1566
-8.250 -0.3532 0.01726 0.01054 -0.1199 0.6896 0.1591
-8.000 -0.3243 0.01703 0.01033 -0.1205 0.6850 0.1612
-7.750 -0.2950 0.01686 0.01016 -0.1210 0.6796 0.1632
-7.500 -0.2655 0.01674 0.00999 -0.1215 0.6740 0.1653
-7.250 -0.2363 0.01665 0.00980 -0.1219 0.6680 0.1668
-7.000 -0.2067 0.01653 0.00964 -0.1224 0.6623 0.1681
-6.750 -0.1769 0.01643 0.00951 -0.1229 0.6556 0.1690
-6.500 -0.1488 0.01610 0.00913 -0.1231 0.6487 0.1704
-6.250 -0.1211 0.01576 0.00876 -0.1233 0.6416 0.1721
-6.000 -0.0923 0.01548 0.00852 -0.1237 0.6336 0.1736
-5.750 -0.0636 0.01529 0.00828 -0.1240 0.6253 0.1748
-5.500 -0.0346 0.01514 0.00810 -0.1243 0.6169 0.1763
-5.250 -0.0056 0.01498 0.00791 -0.1246 0.6077 0.1774
-5.000 0.0231 0.01487 0.00772 -0.1248 0.5994 0.1784
-4.750 0.0524 0.01472 0.00756 -0.1251 0.5914 0.1793
-4.500 0.0813 0.01462 0.00739 -0.1254 0.5839 0.1802
-4.250 0.1103 0.01453 0.00724 -0.1256 0.5773 0.1810
-4.000 0.1396 0.01444 0.00712 -0.1259 0.5705 0.1818
-3.750 0.1685 0.01441 0.00701 -0.1261 0.5637 0.1826
-3.500 0.1976 0.01440 0.00694 -0.1263 0.5574 0.1834
-3.250 0.2268 0.01424 0.00678 -0.1266 0.5518 0.1844
-3.000 0.2555 0.01407 0.00657 -0.1269 0.5466 0.1855
-2.750 0.2842 0.01397 0.00643 -0.1272 0.5413 0.1866
-2.500 0.3134 0.01387 0.00631 -0.1275 0.5364 0.1877
-2.250 0.3429 0.01374 0.00621 -0.1279 0.5322 0.1890
-2.000 0.3724 0.01367 0.00613 -0.1282 0.5282 0.1904
-1.750 0.4017 0.01363 0.00607 -0.1285 0.5242 0.1920
-1.500 0.4310 0.01364 0.00603 -0.1288 0.5201 0.1935
-1.250 0.4607 0.01366 0.00602 -0.1292 0.5164 0.1949
-1.000 0.4904 0.01360 0.00598 -0.1295 0.5138 0.1962
-0.750 0.5201 0.01357 0.00596 -0.1298 0.5106 0.1974
-0.500 0.5495 0.01355 0.00594 -0.1301 0.5071 0.1983
-0.250 0.5788 0.01355 0.00592 -0.1304 0.5036 0.1993
0.000 0.6081 0.01354 0.00588 -0.1307 0.5000 0.2015
0.250 0.6379 0.01361 0.00591 -0.1311 0.4958 0.2041
0.500 0.6673 0.01356 0.00591 -0.1314 0.4931 0.2069
0.750 0.6964 0.01351 0.00591 -0.1317 0.4901 0.2103
1.000 0.7254 0.01349 0.00592 -0.1319 0.4866 0.2145
1.250 0.7545 0.01341 0.00590 -0.1322 0.4832 0.2252
1.500 0.7842 0.01307 0.00588 -0.1331 0.4794 0.3108
1.750 0.8129 0.01321 0.00610 -0.1333 0.4751 0.3545
2.000 0.8414 0.01336 0.00628 -0.1334 0.4713 0.3686
2.250 0.8691 0.01345 0.00642 -0.1333 0.4680 0.3795
2.500 0.8967 0.01355 0.00653 -0.1332 0.4642 0.3859
2.750 0.9239 0.01364 0.00666 -0.1330 0.4600 0.3924
3.000 0.9503 0.01381 0.00681 -0.1327 0.4553 0.3986
3.250 0.9767 0.01403 0.00698 -0.1325 0.4504 0.4030
3.500 1.0028 0.01413 0.00710 -0.1321 0.4463 0.4060
3.750 1.0286 0.01416 0.00719 -0.1318 0.4413 0.4111
4.000 1.0529 0.01429 0.00732 -0.1312 0.4358 0.4153
4.250 1.0759 0.01449 0.00750 -0.1304 0.4300 0.4190
4.500 1.0995 0.01459 0.00766 -0.1297 0.4238 0.4230
4.750 1.1184 0.01477 0.00781 -0.1282 0.4169 0.4260
5.000 1.1366 0.01503 0.00803 -0.1266 0.4100 0.4285
5.250 1.1578 0.01528 0.00829 -0.1256 0.4013 0.4306
5.500 1.1764 0.01562 0.00861 -0.1244 0.3921 0.4350
5.750 1.1955 0.01600 0.00899 -0.1233 0.3808 0.4387
6.000 1.2121 0.01651 0.00948 -0.1220 0.3695 0.4419
6.250 1.2255 0.01721 0.01011 -0.1203 0.3583 0.4448
6.500 1.2409 0.01787 0.01074 -0.1189 0.3475 0.4476
6.750 1.2544 0.01867 0.01149 -0.1174 0.3382 0.4503
7.000 1.2680 0.01950 0.01228 -0.1160 0.3297 0.4533
7.250 1.2812 0.02040 0.01313 -0.1146 0.3227 0.4556
7.500 1.2976 0.02114 0.01390 -0.1137 0.3167 0.4601
7.750 1.3107 0.02210 0.01485 -0.1126 0.3110 0.4639
8.000 1.3241 0.02307 0.01583 -0.1115 0.3061 0.4675
8.250 1.3415 0.02384 0.01665 -0.1108 0.3019 0.4716
8.500 1.3555 0.02484 0.01765 -0.1098 0.2974 0.4756
8.750 1.3668 0.02602 0.01881 -0.1087 0.2929 0.4793
9.000 1.3789 0.02717 0.01996 -0.1077 0.2888 0.4829
9.250 1.3963 0.02800 0.02088 -0.1072 0.2854 0.4898
9.500 1.4102 0.02908 0.02202 -0.1065 0.2817 0.4960
9.750 1.4218 0.03031 0.02326 -0.1056 0.2780 0.5027
10.000 1.4310 0.03172 0.02466 -0.1045 0.2743 0.5098
10.250 1.4445 0.03286 0.02589 -0.1039 0.2712 0.5222
10.500 1.4601 0.03389 0.02702 -0.1034 0.2686 0.5373
10.750 1.4740 0.03505 0.02829 -0.1029 0.2657 0.5589
11.000 1.4855 0.03640 0.02974 -0.1022 0.2627 0.5878
11.250 1.4960 0.03782 0.03127 -0.1015 0.2596 0.6237
11.500 1.5045 0.03934 0.03286 -0.1005 0.2560 0.6613
11.750 1.5173 0.04068 0.03436 -0.1000 0.2538 0.6960
12.000 1.5297 0.04200 0.03580 -0.0995 0.2512 0.7244
12.250 1.5407 0.04346 0.03734 -0.0988 0.2485 0.7468
12.500 1.5492 0.04513 0.03906 -0.0981 0.2457 0.7654
12.750 1.5574 0.04682 0.04077 -0.0974 0.2430 0.7826
13.000 1.5655 0.04841 0.04238 -0.0965 0.2400 0.7992
13.250 1.5755 0.05002 0.04411 -0.0960 0.2382 0.8173
13.500 1.5859 0.05155 0.04577 -0.0955 0.2361 0.8405
13.750 1.5910 0.05286 0.04731 -0.0940 0.2339 1.0000
14.000 1.5993 0.05475 0.04922 -0.0937 0.2316 1.0000
14.250 1.6076 0.05662 0.05108 -0.0933 0.2293 1.0000
14.500 1.6146 0.05859 0.05303 -0.0929 0.2268 1.0000
14.750 1.6236 0.06027 0.05468 -0.0924 0.2243 1.0000
15.000 1.6321 0.06222 0.05670 -0.0922 0.2227 1.0000
15.250 1.6399 0.06423 0.05877 -0.0920 0.2208 1.0000
15.500 1.6469 0.06633 0.06091 -0.0918 0.2188 1.0000
15.750 1.6546 0.06834 0.06294 -0.0916 0.2167 1.0000
16.000 1.6606 0.07051 0.06512 -0.0914 0.2147 1.0000
16.250 1.6666 0.07260 0.06720 -0.0911 0.2125 1.0000
16.500 1.6768 0.07412 0.06868 -0.0907 0.2101 1.0000
16.750 1.6817 0.07653 0.07119 -0.0907 0.2086 1.0000
17.000 1.6855 0.07905 0.07378 -0.0907 0.2067 1.0000
17.250 1.6910 0.08136 0.07614 -0.0907 0.2047 1.0000
17.500 1.6952 0.08381 0.07862 -0.0907 0.2026 1.0000
17.750 1.6992 0.08622 0.08104 -0.0907 0.2006 1.0000
18.000 1.7058 0.08826 0.08307 -0.0907 0.1987 1.0000
18.250 1.7168 0.08966 0.08444 -0.0905 0.1966 1.0000
18.500 1.7194 0.09235 0.08722 -0.0907 0.1953 1.0000
18.750 1.7212 0.09512 0.09008 -0.0909 0.1937 1.0000
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