GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Reynolds number: 500,000 Max Cl/Cd: 99.11 at α=2.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe243-il-500000.txt Download as CSV file: xf-goe243-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 243 (MVA PR.3) 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
------ -------- --------- --------- -------- -------- --------
-9.500 0.1459 0.08951 0.08622 -0.1122 0.8017 0.0427
-9.250 0.1567 0.08721 0.08391 -0.1134 0.7947 0.0433
-9.000 0.1324 0.07678 0.07347 -0.1232 0.7891 0.0466
-8.750 0.1474 0.07552 0.07216 -0.1227 0.7824 0.0468
-8.500 0.1619 0.07407 0.07069 -0.1229 0.7766 0.0471
-8.250 0.1758 0.07243 0.06905 -0.1235 0.7708 0.0474
-8.000 0.1884 0.07051 0.06712 -0.1245 0.7650 0.0479
-7.750 0.1993 0.06823 0.06479 -0.1259 0.7595 0.0486
-7.500 0.1649 0.02664 0.02161 -0.2031 0.7525 0.0413
-7.250 0.1944 0.02435 0.01924 -0.2055 0.7472 0.0408
-7.000 0.2284 0.02236 0.01703 -0.2089 0.7420 0.0404
-6.750 0.2625 0.02074 0.01518 -0.2116 0.7368 0.0402
-6.500 0.2958 0.01940 0.01370 -0.2137 0.7317 0.0401
-6.250 0.3284 0.01834 0.01251 -0.2153 0.7263 0.0402
-6.000 0.3607 0.01755 0.01156 -0.2166 0.7210 0.0405
-5.750 0.3934 0.01696 0.01083 -0.2179 0.7157 0.0410
-5.500 0.4259 0.01644 0.01022 -0.2190 0.7102 0.0414
-5.250 0.4553 0.01567 0.00944 -0.2194 0.7048 0.0418
-5.000 0.4854 0.01516 0.00890 -0.2199 0.6994 0.0422
-4.750 0.5166 0.01478 0.00852 -0.2207 0.6939 0.0428
-4.500 0.5483 0.01442 0.00817 -0.2215 0.6879 0.0434
-4.250 0.5803 0.01411 0.00782 -0.2225 0.6822 0.0442
-4.000 0.6128 0.01386 0.00749 -0.2235 0.6764 0.0449
-3.750 0.6455 0.01355 0.00718 -0.2246 0.6705 0.0458
-3.500 0.6784 0.01328 0.00686 -0.2257 0.6639 0.0466
-3.250 0.7128 0.01294 0.00646 -0.2274 0.6574 0.0480
-3.000 0.7456 0.01270 0.00623 -0.2286 0.6507 0.0498
-2.750 0.7776 0.01253 0.00600 -0.2295 0.6428 0.0517
-2.500 0.8111 0.01227 0.00568 -0.2309 0.6347 0.0541
-2.250 0.8429 0.01210 0.00548 -0.2317 0.6261 0.0572
-2.000 0.8747 0.01196 0.00526 -0.2326 0.6180 0.0619
-1.500 0.9462 0.01093 0.00463 -0.2370 0.6021 0.2462
-1.250 0.9757 0.01095 0.00471 -0.2373 0.5941 0.3039
-1.000 1.0041 0.01105 0.00477 -0.2373 0.5846 0.3210
-0.750 1.0318 0.01118 0.00487 -0.2371 0.5751 0.3329
-0.500 1.0595 0.01132 0.00494 -0.2370 0.5646 0.3417
-0.250 1.0865 0.01146 0.00505 -0.2368 0.5546 0.3513
0.000 1.1135 0.01164 0.00517 -0.2365 0.5436 0.3600
0.250 1.1399 0.01182 0.00530 -0.2362 0.5331 0.3697
0.500 1.1659 0.01203 0.00547 -0.2357 0.5222 0.3785
0.750 1.1920 0.01224 0.00560 -0.2353 0.5120 0.3846
1.000 1.2173 0.01244 0.00574 -0.2348 0.5011 0.3910
1.250 1.2431 0.01262 0.00591 -0.2344 0.4912 0.3968
1.500 1.2674 0.01289 0.00608 -0.2338 0.4812 0.4015
1.750 1.2930 0.01308 0.00624 -0.2333 0.4727 0.4061
2.000 1.3172 0.01332 0.00642 -0.2327 0.4641 0.4114
2.250 1.3415 0.01355 0.00664 -0.2321 0.4567 0.4176
2.500 1.3658 0.01378 0.00685 -0.2314 0.4492 0.4239
3.000 1.4120 0.01431 0.00733 -0.2298 0.4349 0.4366
3.250 1.4340 0.01460 0.00760 -0.2287 0.4278 0.4436
3.500 1.4534 0.01496 0.00790 -0.2273 0.4214 0.4506
3.750 1.4746 0.01517 0.00815 -0.2261 0.4163 0.4579
4.000 1.4939 0.01547 0.00847 -0.2246 0.4106 0.4655
4.250 1.5125 0.01590 0.00884 -0.2230 0.4049 0.4735
4.500 1.5337 0.01622 0.00921 -0.2220 0.4000 0.4815
4.750 1.5547 0.01656 0.00957 -0.2209 0.3946 0.4901
5.000 1.5733 0.01702 0.00999 -0.2195 0.3884 0.4982
5.250 1.5909 0.01752 0.01050 -0.2179 0.3826 0.5054
5.500 1.6120 0.01787 0.01090 -0.2169 0.3780 0.5134
5.750 1.6310 0.01833 0.01134 -0.2156 0.3727 0.5207
6.000 1.6471 0.01892 0.01194 -0.2139 0.3672 0.5268
6.250 1.6659 0.01941 0.01245 -0.2126 0.3625 0.5338
6.500 1.6849 0.01990 0.01294 -0.2115 0.3574 0.5409
6.750 1.7014 0.02050 0.01357 -0.2099 0.3519 0.5466
7.000 1.7156 0.02125 0.01431 -0.2081 0.3464 0.5525
7.250 1.7344 0.02177 0.01488 -0.2070 0.3413 0.5590
7.500 1.7503 0.02246 0.01557 -0.2056 0.3350 0.5642
7.750 1.7620 0.02340 0.01650 -0.2036 0.3286 0.5686
8.000 1.7792 0.02405 0.01719 -0.2024 0.3222 0.5739
8.250 1.7910 0.02505 0.01818 -0.2006 0.3143 0.5793
8.500 1.8040 0.02601 0.01914 -0.1990 0.3062 0.5841
8.750 1.8129 0.02725 0.02037 -0.1970 0.2962 0.5883
9.000 1.8229 0.02846 0.02158 -0.1952 0.2851 0.5929
9.250 1.8280 0.03008 0.02315 -0.1930 0.2718 0.5974
9.500 1.8298 0.03201 0.02500 -0.1906 0.2557 0.6011
9.750 1.8287 0.03422 0.02714 -0.1881 0.2379 0.6043
10.000 1.8262 0.03664 0.02949 -0.1856 0.2218 0.6076
10.250 1.8248 0.03905 0.03186 -0.1833 0.2105 0.6113
10.500 1.8250 0.04140 0.03419 -0.1813 0.2026 0.6151
10.750 1.8277 0.04360 0.03638 -0.1796 0.1974 0.6189
11.000 1.8322 0.04566 0.03848 -0.1781 0.1938 0.6224
11.250 1.8351 0.04791 0.04077 -0.1766 0.1908 0.6257
11.500 1.8367 0.05030 0.04319 -0.1750 0.1881 0.6293
11.750 1.8373 0.05288 0.04580 -0.1735 0.1857 0.6328
12.000 1.8442 0.05482 0.04780 -0.1724 0.1844 0.6368
12.250 1.8501 0.05693 0.04999 -0.1714 0.1833 0.6403
12.500 1.8557 0.05903 0.05217 -0.1703 0.1821 0.6436
12.750 1.8600 0.06132 0.05452 -0.1693 0.1810 0.6469
13.000 1.8643 0.06361 0.05688 -0.1683 0.1800 0.6505
13.250 1.8679 0.06599 0.05932 -0.1673 0.1790 0.6541
13.500 1.8713 0.06844 0.06182 -0.1663 0.1780 0.6573
13.750 1.8748 0.07086 0.06430 -0.1655 0.1770 0.6605
14.000 1.8769 0.07345 0.06695 -0.1646 0.1760 0.6636
14.250 1.8800 0.07588 0.06943 -0.1637 0.1749 0.6672
14.500 1.8830 0.07834 0.07194 -0.1629 0.1740 0.6707
14.750 1.8876 0.08058 0.07422 -0.1621 0.1731 0.6743
15.000 1.8942 0.08253 0.07621 -0.1613 0.1722 0.6778
15.250 1.9021 0.08428 0.07801 -0.1605 0.1715 0.6815
15.500 1.9089 0.08631 0.08012 -0.1600 0.1712 0.6856
15.750 1.9160 0.08830 0.08219 -0.1594 0.1708 0.6897
16.000 1.9237 0.09020 0.08416 -0.1589 0.1705 0.6937
16.250 1.9314 0.09210 0.08615 -0.1585 0.1701 0.6975
16.500 1.9373 0.09427 0.08840 -0.1581 0.1695 0.7015
16.750 1.9431 0.09646 0.09067 -0.1578 0.1687 0.7061
17.000 1.9491 0.09860 0.09289 -0.1575 0.1678 0.7109
17.250 1.9547 0.10080 0.09517 -0.1572 0.1669 0.7156
17.500 1.9599 0.10303 0.09748 -0.1570 0.1659 0.7207
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