GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il) Reynolds number: 1,000,000 Max Cl/Cd: 59.19 at α=3° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe229-il-1000000-n5.txt Download as CSV file: xf-goe229-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.6328 0.11346 0.11105 -0.0722 1.0000 0.0070
-18.500 -0.6606 0.10483 0.10228 -0.0768 1.0000 0.0070
-18.250 -0.6810 0.09770 0.09504 -0.0807 1.0000 0.0070
-18.000 -0.6963 0.09168 0.08892 -0.0840 1.0000 0.0071
-17.750 -0.7087 0.08625 0.08340 -0.0869 1.0000 0.0071
-17.500 -0.7171 0.08114 0.07819 -0.0901 0.9974 0.0072
-17.250 -0.7208 0.07617 0.07313 -0.0941 0.9909 0.0072
-17.000 -0.7214 0.07169 0.06856 -0.0978 0.9829 0.0073
-16.750 -0.7210 0.06764 0.06441 -0.1010 0.9724 0.0074
-16.500 -0.7212 0.06388 0.06055 -0.1036 0.9595 0.0074
-16.250 -0.7228 0.06045 0.05702 -0.1054 0.9451 0.0075
-16.000 -0.7226 0.05747 0.05393 -0.1067 0.9316 0.0076
-15.750 -0.7222 0.05455 0.05088 -0.1081 0.9194 0.0076
-15.500 -0.7223 0.05160 0.04782 -0.1095 0.9072 0.0077
-15.250 -0.7222 0.04863 0.04475 -0.1111 0.8964 0.0079
-15.000 -0.7210 0.04587 0.04188 -0.1126 0.8863 0.0081
-14.750 -0.7181 0.04331 0.03924 -0.1140 0.8761 0.0083
-14.500 -0.7142 0.04097 0.03681 -0.1153 0.8665 0.0085
-14.250 -0.7100 0.03868 0.03443 -0.1166 0.8564 0.0086
-14.000 -0.7039 0.03654 0.03221 -0.1179 0.8471 0.0088
-13.750 -0.6971 0.03449 0.03006 -0.1192 0.8373 0.0090
-13.500 -0.6894 0.03243 0.02793 -0.1206 0.8274 0.0092
-13.250 -0.6806 0.03047 0.02587 -0.1221 0.8177 0.0094
-13.000 -0.6709 0.02855 0.02387 -0.1236 0.8077 0.0096
-12.750 -0.6597 0.02669 0.02192 -0.1255 0.7991 0.0098
-12.500 -0.6422 0.02487 0.02001 -0.1283 0.7908 0.0100
-12.250 -0.6213 0.02315 0.01819 -0.1313 0.7835 0.0102
-12.000 -0.5977 0.02138 0.01634 -0.1349 0.7759 0.0107
-11.750 -0.5714 0.01984 0.01471 -0.1384 0.7694 0.0112
-11.500 -0.5429 0.01855 0.01336 -0.1416 0.7634 0.0117
-11.250 -0.5146 0.01759 0.01232 -0.1439 0.7569 0.0122
-11.000 -0.4872 0.01688 0.01154 -0.1454 0.7509 0.0128
-10.750 -0.4595 0.01626 0.01084 -0.1466 0.7444 0.0133
-10.500 -0.4321 0.01571 0.01022 -0.1477 0.7375 0.0140
-10.250 -0.4040 0.01528 0.00977 -0.1485 0.7316 0.0148
-10.000 -0.3758 0.01491 0.00937 -0.1493 0.7255 0.0157
-9.750 -0.3478 0.01456 0.00895 -0.1500 0.7195 0.0165
-9.500 -0.3193 0.01419 0.00853 -0.1507 0.7143 0.0171
-9.250 -0.2911 0.01384 0.00811 -0.1514 0.7062 0.0177
-9.000 -0.2630 0.01355 0.00778 -0.1520 0.6958 0.0185
-8.750 -0.2351 0.01335 0.00752 -0.1524 0.6841 0.0193
-8.500 -0.2065 0.01315 0.00728 -0.1529 0.6737 0.0202
-8.250 -0.1782 0.01296 0.00702 -0.1533 0.6648 0.0211
-8.000 -0.1496 0.01276 0.00676 -0.1538 0.6549 0.0217
-7.750 -0.1211 0.01258 0.00651 -0.1542 0.6454 0.0221
-7.500 -0.0929 0.01227 0.00612 -0.1547 0.6347 0.0229
-7.250 -0.0644 0.01203 0.00583 -0.1552 0.6238 0.0239
-7.000 -0.0361 0.01187 0.00561 -0.1556 0.6121 0.0247
-6.750 -0.0080 0.01173 0.00539 -0.1559 0.5985 0.0254
-6.500 0.0204 0.01160 0.00519 -0.1563 0.5857 0.0263
-6.250 0.0484 0.01151 0.00500 -0.1566 0.5706 0.0270
-6.000 0.0760 0.01144 0.00483 -0.1568 0.5530 0.0276
-5.750 0.1035 0.01143 0.00470 -0.1569 0.5346 0.0280
-5.500 0.1313 0.01136 0.00454 -0.1571 0.5192 0.0285
-5.250 0.1588 0.01124 0.00428 -0.1574 0.5019 0.0294
-5.000 0.1867 0.01115 0.00409 -0.1576 0.4879 0.0305
-4.750 0.2145 0.01110 0.00396 -0.1578 0.4728 0.0316
-4.500 0.2417 0.01112 0.00386 -0.1579 0.4511 0.0324
-4.250 0.2673 0.01127 0.00381 -0.1577 0.4161 0.0332
-4.000 0.2734 0.01283 0.00444 -0.1543 0.2057 0.0338
-3.750 0.2989 0.01300 0.00446 -0.1541 0.1767 0.0346
-3.250 0.3494 0.01339 0.00458 -0.1536 0.0999 0.0367
-3.000 0.3771 0.01339 0.00455 -0.1537 0.0976 0.0406
-2.750 0.4047 0.01341 0.00454 -0.1538 0.0951 0.0453
-2.500 0.4326 0.01322 0.00447 -0.1543 0.0916 0.0993
-2.250 0.4604 0.01315 0.00444 -0.1545 0.0899 0.1244
-2.000 0.4894 0.01251 0.00423 -0.1557 0.0874 0.2732
-1.750 0.5163 0.01253 0.00430 -0.1558 0.0817 0.3098
-1.250 0.5685 0.01282 0.00457 -0.1555 0.0535 0.3415
-1.000 0.5951 0.01294 0.00470 -0.1554 0.0517 0.3526
-0.750 0.6215 0.01308 0.00484 -0.1553 0.0504 0.3646
-0.500 0.6476 0.01322 0.00498 -0.1552 0.0493 0.3718
-0.250 0.6734 0.01339 0.00513 -0.1549 0.0483 0.3764
0.000 0.6989 0.01357 0.00529 -0.1547 0.0475 0.3800
0.250 0.7243 0.01373 0.00546 -0.1544 0.0468 0.3857
0.500 0.7492 0.01392 0.00564 -0.1540 0.0461 0.3928
0.750 0.7737 0.01412 0.00583 -0.1536 0.0454 0.3967
1.000 0.7978 0.01431 0.00602 -0.1531 0.0448 0.3995
1.250 0.8200 0.01452 0.00623 -0.1522 0.0442 0.4022
1.500 0.8410 0.01474 0.00646 -0.1511 0.0436 0.4052
1.750 0.8627 0.01496 0.00668 -0.1502 0.0432 0.4086
2.000 0.8851 0.01522 0.00693 -0.1494 0.0427 0.4119
2.250 0.9076 0.01550 0.00722 -0.1487 0.0422 0.4152
2.500 0.9298 0.01579 0.00752 -0.1480 0.0418 0.4187
2.750 0.9517 0.01611 0.00784 -0.1473 0.0414 0.4214
3.000 0.9731 0.01644 0.00819 -0.1465 0.0410 0.4243
3.250 0.9941 0.01680 0.00855 -0.1457 0.0407 0.4273
3.500 1.0147 0.01718 0.00894 -0.1448 0.0404 0.4297
3.750 1.0347 0.01759 0.00936 -0.1439 0.0401 0.4318
4.000 1.0544 0.01803 0.00982 -0.1429 0.0399 0.4348
4.250 1.0732 0.01852 0.01035 -0.1419 0.0396 0.4377
4.500 1.0921 0.01902 0.01087 -0.1409 0.0394 0.4406
4.750 1.1106 0.01955 0.01141 -0.1399 0.0393 0.4435
5.000 1.1288 0.02011 0.01200 -0.1389 0.0392 0.4464
5.500 1.1637 0.02135 0.01330 -0.1369 0.0389 0.4527
5.750 1.1805 0.02204 0.01402 -0.1358 0.0388 0.4563
6.000 1.1978 0.02271 0.01472 -0.1349 0.0384 0.4598
6.250 1.2155 0.02336 0.01539 -0.1340 0.0377 0.4631
6.500 1.2329 0.02405 0.01609 -0.1332 0.0371 0.4660
6.750 1.2495 0.02480 0.01687 -0.1323 0.0367 0.4695
7.000 1.2665 0.02554 0.01764 -0.1315 0.0362 0.4734
7.250 1.2828 0.02635 0.01846 -0.1306 0.0358 0.4774
7.500 1.2973 0.02729 0.01944 -0.1296 0.0354 0.4811
8.000 1.3287 0.02905 0.02128 -0.1280 0.0341 0.4899
8.250 1.3445 0.02994 0.02221 -0.1273 0.0332 0.4952
8.500 1.3600 0.03088 0.02316 -0.1266 0.0323 0.5000
8.750 1.3753 0.03182 0.02413 -0.1258 0.0309 0.5047
9.000 1.3894 0.03288 0.02522 -0.1251 0.0276 0.5102
9.250 1.3975 0.03445 0.02673 -0.1239 0.0124 0.5155
9.750 1.4146 0.03769 0.03012 -0.1217 0.0103 0.5270
10.000 1.4237 0.03929 0.03178 -0.1207 0.0097 0.5340
10.250 1.4319 0.04102 0.03359 -0.1198 0.0092 0.5419
10.500 1.4391 0.04289 0.03554 -0.1189 0.0087 0.5520
10.750 1.4457 0.04485 0.03758 -0.1180 0.0082 0.5628
11.000 1.4535 0.04671 0.03952 -0.1172 0.0079 0.5754
11.250 1.4606 0.04867 0.04157 -0.1164 0.0075 0.5896
11.500 1.4677 0.05066 0.04365 -0.1157 0.0072 0.6041
11.750 1.4736 0.05282 0.04588 -0.1151 0.0069 0.6182
12.000 1.4795 0.05498 0.04812 -0.1144 0.0066 0.6315
12.250 1.4847 0.05727 0.05048 -0.1138 0.0064 0.6441
12.500 1.4886 0.05970 0.05298 -0.1132 0.0061 0.6557
12.750 1.4938 0.06202 0.05538 -0.1127 0.0060 0.6675
13.000 1.4977 0.06453 0.05797 -0.1122 0.0059 0.6795
13.250 1.5014 0.06709 0.06063 -0.1118 0.0057 0.6922
13.500 1.5046 0.06973 0.06336 -0.1114 0.0055 0.7058
13.750 1.5068 0.07253 0.06626 -0.1110 0.0054 0.7243
14.000 1.5106 0.07509 0.06915 -0.1109 0.0052 0.8404
14.250 1.5095 0.07771 0.07200 -0.1100 0.0051 1.0000
14.500 1.5104 0.08070 0.07505 -0.1098 0.0049 1.0000
14.750 1.5110 0.08375 0.07815 -0.1095 0.0048 1.0000
15.000 1.5100 0.08705 0.08151 -0.1094 0.0046 1.0000
15.250 1.5086 0.09036 0.08490 -0.1093 0.0045 1.0000
15.500 1.5065 0.09383 0.08843 -0.1092 0.0044 1.0000
15.750 1.5063 0.09704 0.09171 -0.1093 0.0043 1.0000
16.000 1.5043 0.10057 0.09531 -0.1094 0.0043 1.0000
16.250 1.5033 0.10395 0.09875 -0.1095 0.0042 1.0000
16.500 1.5005 0.10762 0.10250 -0.1098 0.0041 1.0000
16.750 1.4983 0.11117 0.10612 -0.1101 0.0040 1.0000
17.000 1.4952 0.11492 0.10994 -0.1106 0.0040 1.0000
17.250 1.4921 0.11869 0.11379 -0.1111 0.0039 1.0000
17.500 1.4892 0.12247 0.11764 -0.1118 0.0038 1.0000
17.750 1.4852 0.12646 0.12170 -0.1126 0.0038 1.0000
18.000 1.4826 0.13025 0.12555 -0.1134 0.0037 1.0000
18.250 1.4780 0.13438 0.12976 -0.1145 0.0036 1.0000
18.500 1.4745 0.13835 0.13381 -0.1155 0.0036 1.0000
18.750 1.4704 0.14246 0.13799 -0.1168 0.0035 1.0000
19.000 1.4660 0.14670 0.14230 -0.1182 0.0035 1.0000
19.250 1.4627 0.15076 0.14643 -0.1197 0.0034 1.0000
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