GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il) Reynolds number: 500,000 Max Cl/Cd: 47.09 at α=2.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe229-il-500000-n5.txt Download as CSV file: xf-goe229-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.750 -0.5366 0.10038 0.09751 -0.0793 1.0000 0.0102
-16.500 -0.5611 0.09141 0.08837 -0.0850 0.9973 0.0103
-16.250 -0.5745 0.08414 0.08093 -0.0904 0.9931 0.0103
-16.000 -0.5838 0.07791 0.07458 -0.0951 0.9871 0.0104
-15.750 -0.5879 0.07253 0.06909 -0.0996 0.9809 0.0106
-15.500 -0.5893 0.06782 0.06428 -0.1036 0.9731 0.0107
-15.250 -0.5882 0.06366 0.06004 -0.1071 0.9641 0.0109
-15.000 -0.5857 0.05999 0.05627 -0.1100 0.9541 0.0110
-14.750 -0.5837 0.05674 0.05292 -0.1122 0.9424 0.0112
-14.500 -0.5820 0.05376 0.04984 -0.1138 0.9304 0.0114
-14.250 -0.5798 0.05102 0.04699 -0.1152 0.9192 0.0115
-14.000 -0.5768 0.04849 0.04433 -0.1164 0.9080 0.0118
-13.750 -0.5733 0.04605 0.04178 -0.1176 0.8972 0.0120
-13.500 -0.5693 0.04380 0.03941 -0.1186 0.8869 0.0122
-13.250 -0.5644 0.04161 0.03710 -0.1197 0.8764 0.0125
-13.000 -0.5583 0.03954 0.03492 -0.1207 0.8668 0.0128
-12.750 -0.5511 0.03761 0.03286 -0.1216 0.8565 0.0131
-12.500 -0.5428 0.03573 0.03086 -0.1226 0.8464 0.0134
-12.250 -0.5344 0.03386 0.02888 -0.1237 0.8373 0.0137
-12.000 -0.5235 0.03208 0.02705 -0.1251 0.8289 0.0141
-11.750 -0.5105 0.03050 0.02539 -0.1264 0.8214 0.0145
-11.500 -0.4970 0.02905 0.02389 -0.1277 0.8136 0.0149
-11.250 -0.4813 0.02765 0.02240 -0.1293 0.8058 0.0153
-11.000 -0.4620 0.02625 0.02092 -0.1314 0.7985 0.0158
-10.750 -0.4411 0.02488 0.01944 -0.1336 0.7910 0.0164
-10.500 -0.4183 0.02355 0.01799 -0.1359 0.7846 0.0170
-10.250 -0.3936 0.02224 0.01657 -0.1386 0.7778 0.0176
-10.000 -0.3667 0.02111 0.01537 -0.1412 0.7715 0.0182
-9.750 -0.3385 0.02032 0.01452 -0.1433 0.7653 0.0189
-9.500 -0.3110 0.01968 0.01381 -0.1448 0.7584 0.0197
-9.250 -0.2841 0.01910 0.01312 -0.1460 0.7520 0.0206
-9.000 -0.2570 0.01851 0.01245 -0.1470 0.7453 0.0215
-8.750 -0.2298 0.01802 0.01184 -0.1479 0.7387 0.0222
-8.500 -0.2034 0.01727 0.01104 -0.1490 0.7330 0.0230
-8.250 -0.1757 0.01680 0.01054 -0.1499 0.7267 0.0239
-8.000 -0.1482 0.01643 0.01010 -0.1505 0.7194 0.0248
-7.750 -0.1205 0.01602 0.00962 -0.1512 0.7105 0.0258
-7.500 -0.0933 0.01565 0.00914 -0.1517 0.7004 0.0268
-7.250 -0.0656 0.01533 0.00872 -0.1522 0.6888 0.0276
-7.000 -0.0378 0.01509 0.00839 -0.1526 0.6780 0.0283
-6.750 -0.0107 0.01441 0.00761 -0.1535 0.6678 0.0296
-6.500 0.0176 0.01399 0.00713 -0.1541 0.6590 0.0306
-6.250 0.0455 0.01370 0.00676 -0.1546 0.6497 0.0317
-6.000 0.0740 0.01341 0.00641 -0.1552 0.6403 0.0328
-5.750 0.1020 0.01316 0.00606 -0.1556 0.6305 0.0338
-5.500 0.1303 0.01294 0.00575 -0.1560 0.6200 0.0347
-5.250 0.1583 0.01277 0.00549 -0.1563 0.6094 0.0355
-5.000 0.1859 0.01261 0.00522 -0.1565 0.5963 0.0364
-4.750 0.2130 0.01244 0.00491 -0.1567 0.5786 0.0378
-4.500 0.2395 0.01237 0.00469 -0.1567 0.5592 0.0393
-4.250 0.2665 0.01231 0.00452 -0.1568 0.5438 0.0410
-4.000 0.2933 0.01230 0.00438 -0.1568 0.5287 0.0431
-3.750 0.3197 0.01233 0.00427 -0.1567 0.5112 0.0457
-3.500 0.3458 0.01232 0.00416 -0.1567 0.4903 0.0544
-3.250 0.3722 0.01208 0.00397 -0.1570 0.4684 0.1142
-3.000 0.3989 0.01140 0.00363 -0.1579 0.4461 0.2560
-2.750 0.4226 0.01153 0.00370 -0.1576 0.4049 0.3078
-2.500 0.4238 0.01338 0.00462 -0.1535 0.2011 0.3236
-2.250 0.4422 0.01406 0.00500 -0.1522 0.1195 0.3409
-2.000 0.4675 0.01427 0.00517 -0.1519 0.1070 0.3553
-1.750 0.4935 0.01443 0.00530 -0.1517 0.1008 0.3654
-1.500 0.5195 0.01459 0.00543 -0.1515 0.0976 0.3748
-1.250 0.5449 0.01478 0.00558 -0.1512 0.0938 0.3818
-1.000 0.5702 0.01496 0.00574 -0.1509 0.0906 0.3892
-0.750 0.5958 0.01513 0.00586 -0.1507 0.0889 0.3938
-0.500 0.6208 0.01530 0.00600 -0.1503 0.0855 0.3987
-0.250 0.6450 0.01551 0.00618 -0.1499 0.0809 0.4054
0.000 0.6669 0.01586 0.00642 -0.1490 0.0569 0.4114
0.250 0.6900 0.01606 0.00662 -0.1483 0.0549 0.4152
0.500 0.7119 0.01627 0.00684 -0.1474 0.0536 0.4186
0.750 0.7333 0.01650 0.00708 -0.1464 0.0526 0.4221
1.000 0.7545 0.01676 0.00735 -0.1454 0.0517 0.4258
1.250 0.7768 0.01704 0.00761 -0.1447 0.0511 0.4289
1.750 0.8211 0.01765 0.00823 -0.1433 0.0497 0.4337
2.000 0.8427 0.01799 0.00859 -0.1425 0.0491 0.4362
2.250 0.8637 0.01837 0.00899 -0.1417 0.0485 0.4390
2.500 0.8838 0.01879 0.00944 -0.1408 0.0479 0.4421
2.750 0.9042 0.01920 0.00986 -0.1399 0.0474 0.4452
3.000 0.9243 0.01963 0.01029 -0.1390 0.0469 0.4480
3.250 0.9439 0.02009 0.01078 -0.1382 0.0463 0.4505
3.500 0.9631 0.02059 0.01131 -0.1372 0.0459 0.4533
3.750 0.9817 0.02112 0.01188 -0.1363 0.0456 0.4562
4.000 0.9999 0.02170 0.01249 -0.1353 0.0452 0.4593
4.250 1.0175 0.02232 0.01313 -0.1343 0.0450 0.4625
4.500 1.0346 0.02299 0.01383 -0.1332 0.0447 0.4658
4.750 1.0512 0.02370 0.01458 -0.1322 0.0445 0.4690
5.000 1.0673 0.02446 0.01540 -0.1311 0.0443 0.4725
5.250 1.0828 0.02528 0.01627 -0.1300 0.0441 0.4761
5.500 1.0976 0.02618 0.01720 -0.1289 0.0439 0.4796
5.750 1.1116 0.02714 0.01821 -0.1278 0.0438 0.4829
6.000 1.1258 0.02811 0.01924 -0.1267 0.0436 0.4863
6.250 1.1399 0.02911 0.02029 -0.1257 0.0436 0.4900
6.500 1.1536 0.03017 0.02141 -0.1247 0.0435 0.4941
6.750 1.1666 0.03130 0.02259 -0.1237 0.0434 0.4984
7.250 1.1929 0.03358 0.02499 -0.1218 0.0428 0.5076
7.500 1.2063 0.03474 0.02621 -0.1210 0.0420 0.5129
7.750 1.2190 0.03597 0.02749 -0.1202 0.0412 0.5182
8.000 1.2310 0.03730 0.02889 -0.1193 0.0406 0.5232
8.250 1.2422 0.03872 0.03038 -0.1185 0.0401 0.5291
8.500 1.2519 0.04029 0.03201 -0.1176 0.0396 0.5352
8.750 1.2640 0.04168 0.03347 -0.1169 0.0390 0.5417
9.000 1.2758 0.04311 0.03498 -0.1163 0.0383 0.5496
9.250 1.2870 0.04464 0.03659 -0.1157 0.0377 0.5580
9.500 1.3001 0.04600 0.03803 -0.1152 0.0366 0.5689
9.750 1.3143 0.04727 0.03934 -0.1148 0.0355 0.5808
10.000 1.3256 0.04882 0.04098 -0.1143 0.0343 0.5939
10.250 1.3374 0.05035 0.04259 -0.1138 0.0328 0.6082
10.500 1.3501 0.05180 0.04411 -0.1135 0.0310 0.6225
10.750 1.3554 0.05403 0.04648 -0.1127 0.0271 0.6350
11.000 1.3698 0.05533 0.04763 -0.1126 0.0132 0.6493
11.250 1.3744 0.05769 0.05009 -0.1119 0.0122 0.6619
11.500 1.3783 0.06014 0.05266 -0.1113 0.0115 0.6748
11.750 1.3822 0.06263 0.05526 -0.1107 0.0109 0.6884
12.000 1.3859 0.06519 0.05794 -0.1103 0.0104 0.7038
12.250 1.3906 0.06768 0.06057 -0.1099 0.0101 0.7251
12.500 1.3953 0.07005 0.06325 -0.1095 0.0097 0.8137
12.750 1.3950 0.07249 0.06589 -0.1085 0.0094 1.0000
13.000 1.3975 0.07529 0.06875 -0.1081 0.0090 1.0000
13.250 1.3993 0.07823 0.07175 -0.1079 0.0086 1.0000
13.500 1.4005 0.08128 0.07485 -0.1077 0.0083 1.0000
13.750 1.4027 0.08421 0.07784 -0.1076 0.0081 1.0000
14.000 1.4042 0.08725 0.08097 -0.1075 0.0079 1.0000
14.250 1.4060 0.09025 0.08403 -0.1074 0.0077 1.0000
14.500 1.4064 0.09347 0.08733 -0.1074 0.0075 1.0000
14.750 1.4075 0.09661 0.09054 -0.1075 0.0073 1.0000
15.000 1.4071 0.09998 0.09399 -0.1076 0.0071 1.0000
15.250 1.4074 0.10328 0.09736 -0.1078 0.0069 1.0000
15.500 1.4060 0.10684 0.10100 -0.1081 0.0068 1.0000
15.750 1.4048 0.11036 0.10459 -0.1084 0.0066 1.0000
16.000 1.4021 0.11417 0.10847 -0.1089 0.0065 1.0000
16.250 1.3990 0.11806 0.11245 -0.1095 0.0064 1.0000
16.500 1.3947 0.12220 0.11668 -0.1103 0.0063 1.0000
16.750 1.3876 0.12683 0.12140 -0.1113 0.0062 1.0000
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