GOE 223 (MVA H.34) AIRFOIL (goe223-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 223 (MVA H.34) AIRFOIL (goe223-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.41 at α=0.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe223-il-1000000-n5.txt Download as CSV file: xf-goe223-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 223 (MVA H.34) 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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7580 0.10450 0.10197 -0.0697 1.0000 0.0114
-18.750 -0.7762 0.09765 0.09501 -0.0737 1.0000 0.0115
-18.500 -0.7892 0.09162 0.08886 -0.0777 0.9880 0.0116
-18.250 -0.7980 0.08627 0.08340 -0.0813 0.9784 0.0117
-18.000 -0.8057 0.08153 0.07856 -0.0840 0.9692 0.0118
-17.750 -0.8134 0.07725 0.07417 -0.0861 0.9599 0.0119
-17.500 -0.8198 0.07315 0.06998 -0.0881 0.9516 0.0121
-17.250 -0.8232 0.06965 0.06640 -0.0897 0.9431 0.0123
-17.000 -0.8243 0.06627 0.06295 -0.0914 0.9349 0.0124
-16.750 -0.8247 0.06308 0.05968 -0.0930 0.9269 0.0126
-16.500 -0.8222 0.06024 0.05677 -0.0944 0.9176 0.0128
-16.250 -0.8200 0.05739 0.05385 -0.0959 0.9075 0.0130
-16.000 -0.8165 0.05479 0.05115 -0.0972 0.8951 0.0132
-15.750 -0.8128 0.05222 0.04848 -0.0985 0.8811 0.0134
-15.500 -0.8080 0.04977 0.04592 -0.0998 0.8677 0.0136
-15.250 -0.8029 0.04740 0.04344 -0.1012 0.8564 0.0139
-15.000 -0.7975 0.04507 0.04100 -0.1025 0.8468 0.0141
-14.750 -0.7917 0.04286 0.03871 -0.1038 0.8386 0.0143
-14.500 -0.7860 0.04066 0.03640 -0.1052 0.8310 0.0146
-14.250 -0.7785 0.03860 0.03425 -0.1065 0.8241 0.0148
-14.000 -0.7704 0.03656 0.03213 -0.1079 0.8166 0.0150
-13.750 -0.7593 0.03474 0.03027 -0.1093 0.8100 0.0152
-13.500 -0.7462 0.03309 0.02856 -0.1107 0.8034 0.0155
-13.250 -0.7323 0.03148 0.02690 -0.1121 0.7980 0.0157
-13.000 -0.7176 0.02989 0.02527 -0.1137 0.7939 0.0160
-12.750 -0.7039 0.02835 0.02368 -0.1152 0.7894 0.0162
-12.500 -0.6846 0.02684 0.02210 -0.1174 0.7850 0.0165
-12.000 -0.6399 0.02394 0.01906 -0.1227 0.7758 0.0172
-11.750 -0.6146 0.02260 0.01764 -0.1255 0.7711 0.0175
-11.500 -0.5877 0.02140 0.01634 -0.1282 0.7666 0.0179
-11.250 -0.5594 0.02033 0.01518 -0.1309 0.7622 0.0181
-11.000 -0.5305 0.01916 0.01396 -0.1338 0.7577 0.0185
-10.750 -0.5019 0.01847 0.01323 -0.1355 0.7527 0.0188
-10.500 -0.4738 0.01794 0.01263 -0.1368 0.7477 0.0191
-10.250 -0.4455 0.01744 0.01209 -0.1379 0.7432 0.0194
-10.000 -0.4170 0.01699 0.01160 -0.1389 0.7381 0.0198
-9.750 -0.3886 0.01657 0.01113 -0.1398 0.7331 0.0202
-9.500 -0.3603 0.01613 0.01062 -0.1407 0.7286 0.0206
-9.250 -0.3317 0.01566 0.01010 -0.1416 0.7237 0.0210
-9.000 -0.3032 0.01525 0.00962 -0.1423 0.7175 0.0213
-8.750 -0.2746 0.01493 0.00923 -0.1430 0.7113 0.0217
-8.500 -0.2456 0.01462 0.00886 -0.1437 0.7044 0.0219
-8.250 -0.2175 0.01399 0.00818 -0.1446 0.6971 0.0223
-8.000 -0.1887 0.01356 0.00770 -0.1454 0.6898 0.0227
-7.750 -0.1599 0.01325 0.00734 -0.1460 0.6806 0.0230
-7.500 -0.1309 0.01298 0.00702 -0.1467 0.6707 0.0235
-7.250 -0.1021 0.01272 0.00669 -0.1472 0.6589 0.0239
-7.000 -0.0735 0.01247 0.00635 -0.1477 0.6438 0.0242
-6.750 -0.0452 0.01226 0.00603 -0.1482 0.6233 0.0246
-6.500 -0.0174 0.01212 0.00574 -0.1485 0.5971 0.0249
-6.250 0.0102 0.01205 0.00552 -0.1488 0.5688 0.0254
-6.000 0.0380 0.01198 0.00532 -0.1491 0.5483 0.0257
-5.750 0.0666 0.01185 0.00509 -0.1495 0.5353 0.0260
-5.500 0.0956 0.01170 0.00488 -0.1499 0.5271 0.0262
-5.250 0.1245 0.01155 0.00466 -0.1504 0.5183 0.0264
-5.000 0.1536 0.01131 0.00433 -0.1510 0.5101 0.0269
-4.750 0.1826 0.01115 0.00411 -0.1514 0.5021 0.0274
-4.500 0.2117 0.01103 0.00394 -0.1519 0.4963 0.0279
-4.250 0.2412 0.01090 0.00378 -0.1523 0.4922 0.0285
-4.000 0.2705 0.01080 0.00364 -0.1528 0.4878 0.0291
-3.750 0.2996 0.01073 0.00353 -0.1532 0.4830 0.0296
-3.500 0.3288 0.01066 0.00342 -0.1535 0.4785 0.0301
-3.250 0.3583 0.01058 0.00331 -0.1540 0.4744 0.0306
-3.000 0.3875 0.01053 0.00322 -0.1543 0.4697 0.0311
-2.750 0.4164 0.01051 0.00316 -0.1547 0.4648 0.0316
-2.500 0.4456 0.01046 0.00308 -0.1550 0.4608 0.0327
-2.250 0.4750 0.01041 0.00301 -0.1554 0.4572 0.0341
-2.000 0.5041 0.01038 0.00296 -0.1558 0.4529 0.0358
-1.750 0.5329 0.01036 0.00292 -0.1561 0.4483 0.0408
-1.500 0.5624 0.01011 0.00282 -0.1568 0.4445 0.1071
-1.250 0.5929 0.00938 0.00257 -0.1581 0.4409 0.2804
-1.000 0.6219 0.00930 0.00259 -0.1586 0.4363 0.3208
-0.750 0.6505 0.00934 0.00264 -0.1588 0.4311 0.3361
-0.500 0.6791 0.00940 0.00269 -0.1591 0.4266 0.3461
-0.250 0.7077 0.00945 0.00274 -0.1593 0.4210 0.3555
0.000 0.7357 0.00955 0.00280 -0.1595 0.4138 0.3623
0.250 0.7637 0.00964 0.00288 -0.1596 0.4056 0.3707
0.500 0.7904 0.00983 0.00298 -0.1596 0.3900 0.3768
0.750 0.8149 0.01015 0.00316 -0.1592 0.3628 0.3820
1.000 0.8248 0.01146 0.00390 -0.1564 0.2550 0.3858
1.250 0.8463 0.01197 0.00424 -0.1556 0.2232 0.3911
1.500 0.8712 0.01223 0.00445 -0.1552 0.2123 0.3969
1.750 0.8967 0.01243 0.00462 -0.1550 0.2049 0.4015
2.000 0.9223 0.01262 0.00479 -0.1547 0.1999 0.4041
2.250 0.9472 0.01285 0.00498 -0.1544 0.1945 0.4067
2.500 0.9724 0.01304 0.00515 -0.1541 0.1901 0.4093
3.000 1.0217 0.01346 0.00553 -0.1533 0.1805 0.4149
3.250 1.0450 0.01371 0.00575 -0.1528 0.1745 0.4179
3.500 1.0635 0.01410 0.00606 -0.1513 0.1566 0.4208
3.750 1.0726 0.01490 0.00667 -0.1484 0.1155 0.4233
4.000 1.0939 0.01524 0.00700 -0.1475 0.1119 0.4262
4.250 1.1153 0.01559 0.00733 -0.1467 0.1088 0.4289
4.500 1.1368 0.01592 0.00768 -0.1459 0.1061 0.4329
4.750 1.1585 0.01624 0.00802 -0.1452 0.1046 0.4367
5.000 1.1800 0.01657 0.00837 -0.1445 0.1040 0.4404
5.250 1.2012 0.01692 0.00874 -0.1437 0.1035 0.4438
5.750 1.2424 0.01770 0.00956 -0.1421 0.1024 0.4511
6.000 1.2625 0.01812 0.01002 -0.1413 0.1020 0.4556
6.250 1.2823 0.01856 0.01049 -0.1404 0.1016 0.4603
6.500 1.3014 0.01905 0.01100 -0.1395 0.1010 0.4647
6.750 1.3194 0.01962 0.01160 -0.1385 0.0997 0.4703
7.000 1.3367 0.02024 0.01225 -0.1374 0.0983 0.4757
7.250 1.3540 0.02087 0.01290 -0.1364 0.0973 0.4807
7.500 1.3708 0.02154 0.01362 -0.1354 0.0961 0.4861
7.750 1.3877 0.02223 0.01435 -0.1344 0.0952 0.4923
8.000 1.4036 0.02300 0.01516 -0.1333 0.0941 0.4983
8.250 1.4193 0.02379 0.01600 -0.1323 0.0930 0.5049
8.500 1.4367 0.02448 0.01675 -0.1315 0.0928 0.5129
8.750 1.4542 0.02518 0.01750 -0.1308 0.0922 0.5216
9.000 1.4709 0.02595 0.01833 -0.1300 0.0914 0.5320
9.250 1.4868 0.02677 0.01922 -0.1291 0.0902 0.5430
9.500 1.5016 0.02770 0.02020 -0.1282 0.0887 0.5544
9.750 1.5150 0.02874 0.02129 -0.1272 0.0867 0.5673
10.000 1.5262 0.02997 0.02256 -0.1260 0.0838 0.5811
10.250 1.5387 0.03111 0.02376 -0.1250 0.0813 0.5961
10.500 1.5324 0.03378 0.02627 -0.1226 0.0519 0.6080
10.750 1.5099 0.03806 0.03050 -0.1192 0.0185 0.6172
11.000 1.5135 0.04017 0.03267 -0.1178 0.0143 0.6311
11.250 1.5205 0.04202 0.03460 -0.1169 0.0130 0.6455
11.500 1.5268 0.04400 0.03665 -0.1159 0.0122 0.6597
11.750 1.5327 0.04605 0.03878 -0.1150 0.0115 0.6733
12.000 1.5380 0.04820 0.04101 -0.1141 0.0108 0.6867
12.250 1.5438 0.05034 0.04324 -0.1134 0.0105 0.7007
12.500 1.5491 0.05257 0.04558 -0.1127 0.0101 0.7176
12.750 1.5541 0.05489 0.04802 -0.1121 0.0096 0.7456
13.000 1.5561 0.05693 0.05049 -0.1110 0.0092 1.0000
13.250 1.5582 0.05962 0.05324 -0.1104 0.0088 1.0000
13.500 1.5592 0.06246 0.05614 -0.1098 0.0085 1.0000
13.750 1.5621 0.06514 0.05888 -0.1093 0.0083 1.0000
14.000 1.5649 0.06785 0.06165 -0.1089 0.0081 1.0000
14.250 1.5667 0.07071 0.06457 -0.1086 0.0079 1.0000
14.500 1.5680 0.07361 0.06753 -0.1082 0.0077 1.0000
14.750 1.5694 0.07651 0.07049 -0.1079 0.0074 1.0000
15.000 1.5698 0.07956 0.07360 -0.1077 0.0072 1.0000
15.250 1.5700 0.08266 0.07676 -0.1075 0.0071 1.0000
15.500 1.5703 0.08575 0.07990 -0.1073 0.0069 1.0000
15.750 1.5691 0.08906 0.08328 -0.1072 0.0067 1.0000
16.000 1.5679 0.09231 0.08658 -0.1071 0.0065 1.0000
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