GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il) Reynolds number: 200,000 Max Cl/Cd: 40.89 at α=-0.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe229-il-200000-n5.txt Download as CSV file: xf-goe229-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 229 (MVA H.39) AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.2657 0.08138 0.07768 -0.1070 0.9486 0.0196
-12.750 -0.3119 0.06818 0.06415 -0.1175 0.9407 0.0193
-12.500 -0.3338 0.06131 0.05706 -0.1229 0.9291 0.0194
-12.250 -0.3478 0.05596 0.05149 -0.1270 0.9179 0.0195
-12.000 -0.3577 0.05151 0.04681 -0.1302 0.9067 0.0198
-11.750 -0.3648 0.04779 0.04288 -0.1327 0.8942 0.0201
-11.500 -0.3692 0.04437 0.03922 -0.1351 0.8834 0.0206
-11.250 -0.3716 0.04115 0.03573 -0.1373 0.8734 0.0213
-11.000 -0.3732 0.03822 0.03248 -0.1395 0.8630 0.0219
-10.750 -0.3679 0.03587 0.02987 -0.1414 0.8551 0.0225
-10.500 -0.3533 0.03433 0.02829 -0.1426 0.8467 0.0230
-10.250 -0.3360 0.03282 0.02666 -0.1443 0.8398 0.0236
-10.000 -0.3181 0.03145 0.02516 -0.1453 0.8327 0.0243
-9.750 -0.2991 0.03014 0.02369 -0.1460 0.8256 0.0251
-9.500 -0.2783 0.02894 0.02229 -0.1467 0.8195 0.0263
-9.250 -0.2572 0.02790 0.02104 -0.1474 0.8119 0.0276
-9.000 -0.2350 0.02675 0.01972 -0.1477 0.8056 0.0287
-8.750 -0.2137 0.02569 0.01867 -0.1475 0.7990 0.0297
-8.500 -0.1909 0.02482 0.01776 -0.1477 0.7924 0.0307
-8.000 -0.1427 0.02331 0.01608 -0.1482 0.7798 0.0337
-7.750 -0.1176 0.02265 0.01529 -0.1485 0.7732 0.0350
-7.500 -0.0920 0.02205 0.01457 -0.1488 0.7668 0.0359
-7.250 -0.0698 0.02100 0.01355 -0.1488 0.7594 0.0375
-7.000 -0.0440 0.02023 0.01273 -0.1495 0.7533 0.0393
-6.750 -0.0182 0.01959 0.01205 -0.1501 0.7462 0.0409
-6.500 0.0088 0.01897 0.01134 -0.1508 0.7395 0.0423
-6.250 0.0366 0.01841 0.01068 -0.1515 0.7334 0.0438
-6.000 0.0641 0.01796 0.01013 -0.1522 0.7261 0.0454
-5.750 0.0926 0.01732 0.00935 -0.1532 0.7196 0.0474
-5.500 0.1207 0.01681 0.00875 -0.1540 0.7119 0.0494
-5.250 0.1492 0.01640 0.00821 -0.1546 0.7034 0.0517
-5.000 0.1771 0.01608 0.00777 -0.1550 0.6938 0.0547
-4.750 0.2055 0.01577 0.00732 -0.1554 0.6842 0.0603
-4.500 0.2333 0.01517 0.00687 -0.1562 0.6732 0.0987
-4.250 0.2617 0.01400 0.00619 -0.1578 0.6629 0.2432
-4.000 0.2894 0.01379 0.00615 -0.1582 0.6523 0.3130
-3.750 0.3173 0.01382 0.00615 -0.1583 0.6427 0.3445
-3.500 0.3452 0.01390 0.00611 -0.1583 0.6333 0.3612
-3.250 0.3726 0.01400 0.00615 -0.1582 0.6222 0.3753
-3.000 0.3995 0.01412 0.00618 -0.1580 0.6104 0.3861
-2.750 0.4264 0.01425 0.00614 -0.1579 0.5982 0.3969
-2.500 0.4526 0.01437 0.00619 -0.1576 0.5851 0.4035
-2.250 0.4787 0.01454 0.00618 -0.1573 0.5699 0.4134
-2.000 0.5029 0.01478 0.00635 -0.1566 0.5524 0.4223
-1.750 0.5280 0.01501 0.00637 -0.1562 0.5361 0.4309
-1.500 0.5528 0.01516 0.00647 -0.1557 0.5229 0.4356
-1.250 0.5773 0.01533 0.00652 -0.1552 0.5086 0.4393
-1.000 0.6008 0.01551 0.00655 -0.1545 0.4893 0.4427
-0.750 0.6235 0.01574 0.00659 -0.1538 0.4658 0.4464
-0.500 0.6459 0.01598 0.00664 -0.1530 0.4424 0.4496
-0.250 0.6661 0.01629 0.00678 -0.1519 0.4080 0.4520
0.250 0.6672 0.01913 0.00837 -0.1436 0.1973 0.4564
0.750 0.6878 0.02062 0.00940 -0.1384 0.1088 0.4626
1.000 0.7075 0.02101 0.00972 -0.1374 0.1036 0.4659
1.250 0.7289 0.02132 0.01004 -0.1367 0.1008 0.4684
1.500 0.7500 0.02166 0.01039 -0.1359 0.0983 0.4711
1.750 0.7707 0.02205 0.01078 -0.1351 0.0960 0.4744
2.000 0.7904 0.02249 0.01121 -0.1343 0.0935 0.4781
2.250 0.8092 0.02300 0.01168 -0.1333 0.0909 0.4818
2.500 0.8298 0.02340 0.01206 -0.1326 0.0889 0.4850
2.750 0.8498 0.02381 0.01251 -0.1319 0.0862 0.4878
3.000 0.8691 0.02429 0.01301 -0.1310 0.0836 0.4910
3.250 0.8883 0.02479 0.01352 -0.1302 0.0819 0.4947
3.500 0.9064 0.02538 0.01411 -0.1293 0.0637 0.4988
3.750 0.9199 0.02627 0.01490 -0.1280 0.0607 0.5027
4.000 0.9370 0.02692 0.01562 -0.1270 0.0597 0.5062
4.250 0.9537 0.02763 0.01637 -0.1261 0.0591 0.5100
4.500 0.9703 0.02836 0.01716 -0.1251 0.0586 0.5141
4.750 0.9866 0.02915 0.01798 -0.1242 0.0582 0.5184
5.000 1.0022 0.02998 0.01888 -0.1233 0.0579 0.5223
5.250 1.0172 0.03088 0.01987 -0.1223 0.0575 0.5264
5.500 1.0315 0.03185 0.02091 -0.1213 0.0571 0.5314
5.750 1.0453 0.03290 0.02203 -0.1204 0.0566 0.5368
6.000 1.0583 0.03401 0.02324 -0.1194 0.0562 0.5417
6.250 1.0706 0.03520 0.02453 -0.1183 0.0559 0.5471
6.500 1.0825 0.03646 0.02587 -0.1173 0.0556 0.5531
6.750 1.0952 0.03766 0.02716 -0.1165 0.0554 0.5587
7.000 1.1077 0.03890 0.02849 -0.1156 0.0554 0.5649
7.250 1.1196 0.04022 0.02990 -0.1148 0.0553 0.5719
7.500 1.1311 0.04159 0.03137 -0.1140 0.0552 0.5790
7.750 1.1423 0.04302 0.03290 -0.1132 0.0552 0.5874
8.000 1.1530 0.04453 0.03451 -0.1124 0.0551 0.5963
8.250 1.1636 0.04608 0.03616 -0.1117 0.0551 0.6064
8.500 1.1736 0.04771 0.03791 -0.1110 0.0551 0.6167
8.750 1.1832 0.04940 0.03970 -0.1104 0.0551 0.6282
9.000 1.1925 0.05115 0.04156 -0.1097 0.0550 0.6396
9.250 1.2008 0.05304 0.04356 -0.1091 0.0546 0.6517
9.500 1.2073 0.05515 0.04579 -0.1084 0.0538 0.6646
9.750 1.2109 0.05761 0.04838 -0.1077 0.0528 0.6782
10.000 1.2105 0.06056 0.05150 -0.1069 0.0520 0.6921
10.250 1.2184 0.06260 0.05368 -0.1064 0.0512 0.7107
10.500 1.2254 0.06473 0.05599 -0.1060 0.0505 0.7362
10.750 1.2258 0.06661 0.05826 -0.1045 0.0498 0.9172
11.000 1.2280 0.06930 0.06104 -0.1040 0.0490 1.0000
11.250 1.2276 0.07253 0.06436 -0.1037 0.0481 1.0000
11.500 1.2345 0.07489 0.06681 -0.1035 0.0468 1.0000
11.750 1.2403 0.07739 0.06939 -0.1034 0.0456 1.0000
12.000 1.2434 0.08027 0.07235 -0.1033 0.0447 1.0000
12.250 1.2442 0.08348 0.07565 -0.1032 0.0439 1.0000
12.500 1.2530 0.08562 0.07787 -0.1032 0.0426 1.0000
12.750 1.2601 0.08799 0.08031 -0.1032 0.0410 1.0000
13.000 1.2639 0.09084 0.08324 -0.1032 0.0396 1.0000
13.250 1.2757 0.09258 0.08506 -0.1033 0.0376 1.0000
13.500 1.2839 0.09483 0.08738 -0.1034 0.0357 1.0000
13.750 1.2934 0.09690 0.08952 -0.1035 0.0333 1.0000
14.000 1.3017 0.09913 0.09186 -0.1036 0.0296 1.0000
14.250 1.3132 0.10089 0.09355 -0.1038 0.0172 1.0000
14.500 1.3169 0.10375 0.09637 -0.1041 0.0155 1.0000
14.750 1.3181 0.10697 0.09966 -0.1044 0.0148 1.0000
15.000 1.3185 0.11035 0.10314 -0.1048 0.0143 1.0000
15.250 1.3188 0.11378 0.10665 -0.1053 0.0139 1.0000
15.500 1.3180 0.11741 0.11036 -0.1059 0.0135 1.0000
15.750 1.3170 0.12110 0.11415 -0.1066 0.0132 1.0000
16.000 1.3160 0.12483 0.11797 -0.1075 0.0129 1.0000
16.250 1.3152 0.12857 0.12182 -0.1084 0.0126 1.0000
16.500 1.3136 0.13245 0.12581 -0.1095 0.0124 1.0000
16.750 1.3110 0.13659 0.13006 -0.1107 0.0120 1.0000
17.000 1.3078 0.14087 0.13446 -0.1122 0.0117 1.0000
17.250 1.3037 0.14536 0.13906 -0.1138 0.0115 1.0000
17.500 1.2985 0.15012 0.14393 -0.1157 0.0112 1.0000
17.750 1.2935 0.15495 0.14889 -0.1178 0.0111 1.0000
18.000 1.2875 0.16000 0.15404 -0.1200 0.0109 1.0000
18.250 1.2817 0.16508 0.15923 -0.1225 0.0108 1.0000
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