GOE 241 (MVA PR.1) AIRFOIL (goe241-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 241 (MVA PR.1) AIRFOIL (goe241-il) Reynolds number: 1,000,000 Max Cl/Cd: 113.23 at α=3° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe241-il-1000000-n5.txt Download as CSV file: xf-goe241-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 241 (MVA PR.1) 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
------ -------- --------- --------- -------- -------- --------
-14.000 -0.4232 0.05536 0.05205 -0.1283 0.8067 0.0235
-13.750 -0.4422 0.04876 0.04525 -0.1345 0.7981 0.0236
-13.500 -0.4475 0.04432 0.04065 -0.1388 0.7903 0.0237
-13.250 -0.4479 0.04062 0.03683 -0.1427 0.7827 0.0237
-13.000 -0.4450 0.03754 0.03361 -0.1460 0.7748 0.0238
-12.750 -0.4427 0.03447 0.03043 -0.1496 0.7685 0.0239
-12.500 -0.4303 0.03148 0.02731 -0.1546 0.7619 0.0240
-12.250 -0.4105 0.02915 0.02489 -0.1592 0.7557 0.0242
-12.000 -0.3859 0.02720 0.02284 -0.1636 0.7508 0.0243
-11.750 -0.3582 0.02548 0.02106 -0.1679 0.7454 0.0245
-11.500 -0.3284 0.02398 0.01947 -0.1719 0.7397 0.0246
-11.250 -0.2972 0.02266 0.01806 -0.1757 0.7346 0.0248
-11.000 -0.2645 0.02144 0.01678 -0.1794 0.7298 0.0249
-10.750 -0.2311 0.02033 0.01560 -0.1829 0.7237 0.0251
-10.500 -0.1975 0.01934 0.01450 -0.1862 0.7169 0.0253
-10.250 -0.1634 0.01841 0.01349 -0.1892 0.7111 0.0255
-10.000 -0.1292 0.01756 0.01256 -0.1921 0.7048 0.0257
-9.750 -0.0954 0.01681 0.01171 -0.1946 0.6980 0.0259
-9.500 -0.0620 0.01614 0.01096 -0.1968 0.6919 0.0262
-9.250 -0.0294 0.01559 0.01032 -0.1985 0.6840 0.0264
-9.000 0.0026 0.01514 0.00978 -0.1999 0.6759 0.0267
-8.750 0.0347 0.01472 0.00927 -0.2013 0.6666 0.0269
-8.500 0.0665 0.01434 0.00879 -0.2025 0.6574 0.0271
-8.250 0.0984 0.01397 0.00834 -0.2037 0.6482 0.0273
-8.000 0.1299 0.01365 0.00793 -0.2048 0.6388 0.0274
-7.750 0.1621 0.01324 0.00744 -0.2061 0.6285 0.0277
-7.500 0.1940 0.01289 0.00702 -0.2073 0.6184 0.0280
-7.250 0.2255 0.01263 0.00669 -0.2083 0.6069 0.0283
-7.000 0.2567 0.01242 0.00641 -0.2092 0.5959 0.0285
-6.750 0.2875 0.01226 0.00617 -0.2099 0.5837 0.0288
-6.500 0.3184 0.01210 0.00594 -0.2106 0.5710 0.0291
-6.250 0.3491 0.01197 0.00572 -0.2113 0.5594 0.0295
-6.000 0.3796 0.01186 0.00552 -0.2120 0.5480 0.0298
-5.750 0.4105 0.01172 0.00532 -0.2126 0.5378 0.0302
-5.500 0.4408 0.01164 0.00515 -0.2132 0.5263 0.0306
-5.250 0.4711 0.01156 0.00499 -0.2138 0.5149 0.0309
-5.000 0.5014 0.01149 0.00484 -0.2143 0.5059 0.0313
-4.750 0.5320 0.01138 0.00468 -0.2149 0.4976 0.0318
-4.500 0.5623 0.01131 0.00455 -0.2155 0.4898 0.0324
-4.250 0.5925 0.01125 0.00446 -0.2159 0.4821 0.0330
-4.000 0.6222 0.01124 0.00438 -0.2163 0.4746 0.0336
-3.750 0.6524 0.01119 0.00429 -0.2168 0.4695 0.0342
-3.500 0.6824 0.01115 0.00422 -0.2172 0.4632 0.0349
-3.250 0.7116 0.01117 0.00417 -0.2175 0.4559 0.0355
-3.000 0.7416 0.01113 0.00410 -0.2179 0.4506 0.0364
-2.750 0.7712 0.01112 0.00406 -0.2182 0.4454 0.0374
-2.500 0.8006 0.01113 0.00404 -0.2185 0.4407 0.0386
-2.250 0.8295 0.01117 0.00403 -0.2187 0.4362 0.0398
-2.000 0.8591 0.01116 0.00401 -0.2191 0.4331 0.0414
-1.750 0.8885 0.01116 0.00401 -0.2194 0.4293 0.0433
-1.500 0.9173 0.01120 0.00403 -0.2195 0.4247 0.0452
-1.250 0.9458 0.01126 0.00405 -0.2197 0.4202 0.0473
-1.000 0.9743 0.01131 0.00408 -0.2198 0.4166 0.0500
-0.750 1.0033 0.01133 0.00410 -0.2200 0.4142 0.0527
-0.500 1.0321 0.01136 0.00413 -0.2202 0.4114 0.0568
-0.250 1.0606 0.01140 0.00417 -0.2204 0.4083 0.0631
0.000 1.0892 0.01141 0.00422 -0.2206 0.4047 0.0879
0.250 1.1212 0.01100 0.00423 -0.2221 0.4006 0.2928
0.500 1.1491 0.01105 0.00433 -0.2222 0.3971 0.3203
0.750 1.1771 0.01112 0.00443 -0.2223 0.3938 0.3395
1.000 1.2045 0.01122 0.00453 -0.2223 0.3904 0.3550
1.250 1.2314 0.01134 0.00466 -0.2221 0.3867 0.3693
1.500 1.2575 0.01150 0.00481 -0.2219 0.3826 0.3788
1.750 1.2840 0.01163 0.00494 -0.2217 0.3792 0.3878
2.000 1.3106 0.01175 0.00507 -0.2215 0.3750 0.3978
2.250 1.3361 0.01192 0.00523 -0.2211 0.3698 0.4065
2.500 1.3606 0.01214 0.00541 -0.2206 0.3646 0.4143
2.750 1.3860 0.01229 0.00558 -0.2202 0.3606 0.4225
3.000 1.4109 0.01246 0.00574 -0.2198 0.3559 0.4280
3.500 1.4563 0.01291 0.00615 -0.2181 0.3453 0.4371
3.750 1.4767 0.01312 0.00636 -0.2167 0.3395 0.4425
4.000 1.4953 0.01345 0.00665 -0.2152 0.3315 0.4478
4.250 1.5162 0.01376 0.00693 -0.2141 0.3229 0.4521
4.500 1.5344 0.01422 0.00733 -0.2126 0.3101 0.4569
4.750 1.5498 0.01483 0.00784 -0.2107 0.2920 0.4614
5.000 1.5623 0.01560 0.00849 -0.2084 0.2719 0.4657
5.250 1.5754 0.01635 0.00915 -0.2062 0.2565 0.4697
5.500 1.5907 0.01700 0.00976 -0.2045 0.2466 0.4733
5.750 1.6065 0.01763 0.01037 -0.2028 0.2389 0.4782
6.000 1.6236 0.01822 0.01095 -0.2014 0.2335 0.4830
6.250 1.6414 0.01876 0.01150 -0.2002 0.2299 0.4873
6.500 1.6589 0.01934 0.01207 -0.1989 0.2266 0.4910
6.750 1.6753 0.01999 0.01272 -0.1975 0.2234 0.4941
7.000 1.6917 0.02065 0.01340 -0.1962 0.2201 0.4985
7.250 1.7089 0.02128 0.01406 -0.1950 0.2179 0.5030
7.500 1.7262 0.02191 0.01471 -0.1939 0.2163 0.5071
7.750 1.7431 0.02258 0.01540 -0.1928 0.2146 0.5107
8.000 1.7588 0.02333 0.01618 -0.1915 0.2127 0.5140
8.250 1.7746 0.02411 0.01698 -0.1903 0.2110 0.5176
8.500 1.7889 0.02499 0.01789 -0.1890 0.2092 0.5211
8.750 1.8031 0.02589 0.01883 -0.1877 0.2074 0.5247
9.000 1.8162 0.02689 0.01986 -0.1864 0.2055 0.5283
9.250 1.8297 0.02788 0.02088 -0.1851 0.2040 0.5315
9.500 1.8421 0.02898 0.02200 -0.1838 0.2025 0.5340
9.750 1.8564 0.02994 0.02301 -0.1827 0.2018 0.5370
10.000 1.8707 0.03091 0.02405 -0.1817 0.2010 0.5404
10.250 1.8849 0.03190 0.02509 -0.1807 0.1998 0.5438
10.500 1.8976 0.03304 0.02627 -0.1796 0.1981 0.5469
10.750 1.9095 0.03426 0.02753 -0.1784 0.1964 0.5495
11.000 1.9204 0.03558 0.02889 -0.1773 0.1948 0.5520
11.250 1.9298 0.03704 0.03039 -0.1760 0.1930 0.5547
11.500 1.9389 0.03856 0.03196 -0.1748 0.1914 0.5577
11.750 1.9465 0.04024 0.03368 -0.1735 0.1895 0.5604
12.000 1.9533 0.04203 0.03551 -0.1723 0.1876 0.5630
12.250 1.9616 0.04369 0.03724 -0.1712 0.1864 0.5656
12.500 1.9723 0.04517 0.03877 -0.1703 0.1857 0.5684
13.000 1.9909 0.04838 0.04211 -0.1685 0.1824 0.5739
13.250 1.9971 0.05034 0.04412 -0.1675 0.1799 0.5766
13.500 2.0021 0.05244 0.04627 -0.1664 0.1777 0.5792
13.750 2.0050 0.05479 0.04866 -0.1654 0.1754 0.5818
14.000 2.0052 0.05746 0.05138 -0.1642 0.1728 0.5844
14.250 2.0108 0.05954 0.05352 -0.1634 0.1709 0.5873
14.500 2.0137 0.06197 0.05602 -0.1625 0.1681 0.5901
14.750 2.0133 0.06478 0.05887 -0.1616 0.1633 0.5930
15.000 2.0080 0.06818 0.06229 -0.1605 0.1583 0.5956
15.250 1.9999 0.07196 0.06609 -0.1595 0.1498 0.5981
15.500 1.9710 0.07820 0.07228 -0.1580 0.1339 0.5994
15.750 1.9346 0.08560 0.07964 -0.1567 0.1171 0.6003
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