USA 34 AIRFOIL (usa34-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: USA 34 AIRFOIL (usa34-il) Reynolds number: 1,000,000 Max Cl/Cd: 104.83 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-usa34-il-1000000.txt Download as CSV file: xf-usa34-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: USA 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.3492 0.14534 0.14326 -0.0810 0.9929 0.0230
-18.750 -0.4316 0.12562 0.12332 -0.0911 0.9919 0.0240
-18.500 -0.4461 0.11826 0.11587 -0.0961 0.9904 0.0244
-18.250 -0.4538 0.11196 0.10949 -0.1008 0.9890 0.0248
-18.000 -0.4562 0.10654 0.10400 -0.1053 0.9876 0.0251
-17.750 -0.4602 0.10078 0.09817 -0.1101 0.9862 0.0255
-17.500 -0.4619 0.09525 0.09255 -0.1151 0.9849 0.0258
-17.250 -0.4587 0.09054 0.08778 -0.1197 0.9837 0.0259
-17.000 -0.4562 0.08565 0.08283 -0.1248 0.9825 0.0263
-16.750 -0.4409 0.08284 0.08002 -0.1286 0.9816 0.0266
-16.500 -0.4438 0.07999 0.07717 -0.1289 0.9749 0.0269
-16.250 -0.4375 0.07630 0.07346 -0.1326 0.9710 0.0271
-16.000 -0.4451 0.07282 0.06996 -0.1336 0.9588 0.0273
-15.750 -0.4463 0.06879 0.06589 -0.1367 0.9444 0.0276
-15.500 -0.4373 0.06339 0.06041 -0.1443 0.9346 0.0279
-15.250 -0.4245 0.05635 0.05325 -0.1564 0.9259 0.0283
-15.000 -0.4128 0.04861 0.04526 -0.1709 0.9028 0.0285
-14.750 -0.5174 0.02672 0.02260 -0.1988 0.8457 0.0279
-14.500 -0.5075 0.02400 0.01964 -0.2017 0.8305 0.0282
-14.250 -0.5026 0.02252 0.01798 -0.2008 0.8178 0.0284
-14.000 -0.4993 0.02146 0.01681 -0.1984 0.8081 0.0286
-13.750 -0.4954 0.02063 0.01583 -0.1954 0.7989 0.0289
-13.500 -0.4916 0.01997 0.01509 -0.1918 0.7917 0.0291
-13.250 -0.4822 0.01936 0.01438 -0.1892 0.7851 0.0294
-13.000 -0.4696 0.01883 0.01374 -0.1870 0.7795 0.0296
-12.750 -0.4588 0.01819 0.01301 -0.1844 0.7750 0.0299
-12.500 -0.4527 0.01735 0.01210 -0.1811 0.7711 0.0304
-12.250 -0.4412 0.01670 0.01138 -0.1786 0.7671 0.0309
-12.000 -0.4266 0.01618 0.01078 -0.1763 0.7630 0.0313
-11.750 -0.4092 0.01574 0.01024 -0.1746 0.7587 0.0317
-11.500 -0.3910 0.01532 0.00975 -0.1729 0.7557 0.0321
-11.250 -0.3735 0.01489 0.00928 -0.1709 0.7531 0.0326
-11.000 -0.3545 0.01454 0.00887 -0.1692 0.7501 0.0331
-10.750 -0.3350 0.01420 0.00847 -0.1676 0.7469 0.0334
-10.500 -0.3172 0.01376 0.00796 -0.1657 0.7436 0.0341
-10.250 -0.2980 0.01334 0.00746 -0.1640 0.7401 0.0350
-10.000 -0.2756 0.01298 0.00704 -0.1630 0.7368 0.0359
-9.750 -0.2559 0.01266 0.00668 -0.1612 0.7347 0.0366
-9.500 -0.2353 0.01237 0.00635 -0.1596 0.7321 0.0374
-9.250 -0.2151 0.01202 0.00597 -0.1580 0.7294 0.0389
-9.000 -0.1948 0.01165 0.00558 -0.1564 0.7266 0.0413
-8.750 -0.1754 0.01119 0.00518 -0.1547 0.7239 0.0513
-8.500 -0.1493 0.01112 0.00517 -0.1542 0.7211 0.0666
-8.250 -0.1201 0.01112 0.00514 -0.1542 0.7180 0.0706
-8.000 -0.0942 0.01111 0.00514 -0.1535 0.7160 0.0736
-7.750 -0.0692 0.01111 0.00512 -0.1526 0.7138 0.0754
-7.500 -0.0462 0.01098 0.00498 -0.1514 0.7112 0.0771
-7.250 -0.0231 0.01087 0.00487 -0.1502 0.7084 0.0786
-7.000 0.0013 0.01081 0.00480 -0.1493 0.7055 0.0801
-6.750 0.0260 0.01077 0.00471 -0.1484 0.7026 0.0813
-6.500 0.0531 0.01077 0.00466 -0.1480 0.6991 0.0826
-6.250 0.0783 0.01075 0.00461 -0.1472 0.6963 0.0833
-6.000 0.0977 0.01050 0.00436 -0.1453 0.6936 0.0845
-5.750 0.1183 0.01032 0.00419 -0.1436 0.6903 0.0857
-5.500 0.1399 0.01020 0.00406 -0.1420 0.6869 0.0867
-5.250 0.1611 0.01011 0.00394 -0.1404 0.6833 0.0876
-5.000 0.1847 0.01004 0.00383 -0.1393 0.6790 0.0884
-4.750 0.2034 0.00992 0.00371 -0.1371 0.6759 0.0893
-4.500 0.2217 0.00980 0.00358 -0.1349 0.6718 0.0900
-4.250 0.2414 0.00971 0.00347 -0.1329 0.6670 0.0907
-4.000 0.2611 0.00965 0.00336 -0.1310 0.6620 0.0912
-3.750 0.2821 0.00959 0.00328 -0.1293 0.6574 0.0917
-3.500 0.3015 0.00941 0.00310 -0.1273 0.6519 0.0931
-3.250 0.3200 0.00931 0.00298 -0.1252 0.6453 0.0942
-3.000 0.3378 0.00925 0.00290 -0.1228 0.6382 0.0952
-2.750 0.3561 0.00920 0.00283 -0.1206 0.6292 0.0963
-2.500 0.3730 0.00921 0.00280 -0.1181 0.6194 0.0976
-2.250 0.3893 0.00923 0.00277 -0.1155 0.6065 0.0984
-2.000 0.4059 0.00928 0.00276 -0.1130 0.5923 0.0995
-1.750 0.4203 0.00938 0.00278 -0.1100 0.5774 0.1003
-1.500 0.4339 0.00948 0.00281 -0.1069 0.5639 0.1021
-1.250 0.4484 0.00958 0.00286 -0.1040 0.5516 0.1039
-1.000 0.4669 0.00965 0.00290 -0.1020 0.5425 0.1061
-0.750 0.4837 0.00976 0.00297 -0.0996 0.5342 0.1081
-0.500 0.5031 0.00983 0.00302 -0.0978 0.5281 0.1111
-0.250 0.5222 0.00987 0.00308 -0.0959 0.5224 0.1169
0.000 0.5396 0.00997 0.00317 -0.0937 0.5164 0.1245
0.250 0.5592 0.01005 0.00326 -0.0920 0.5114 0.1330
0.500 0.5810 0.01008 0.00333 -0.0907 0.5074 0.1423
0.750 0.6017 0.01018 0.00342 -0.0892 0.5033 0.1477
1.000 0.6199 0.01028 0.00352 -0.0872 0.4990 0.1551
1.250 0.6374 0.01044 0.00366 -0.0851 0.4939 0.1601
1.500 0.6602 0.01048 0.00372 -0.0841 0.4912 0.1653
1.750 0.6824 0.01052 0.00381 -0.0830 0.4879 0.1729
2.000 0.7024 0.01063 0.00392 -0.0815 0.4833 0.1786
2.250 0.7203 0.01078 0.00407 -0.0796 0.4788 0.1899
2.500 0.7397 0.01091 0.00424 -0.0780 0.4746 0.2077
2.750 0.7633 0.01092 0.00438 -0.0773 0.4717 0.2404
3.000 0.7864 0.01099 0.00453 -0.0765 0.4687 0.2681
3.250 0.8082 0.01111 0.00470 -0.0755 0.4655 0.2869
3.500 0.8273 0.01131 0.00490 -0.0740 0.4609 0.3013
4.000 0.8712 0.01163 0.00529 -0.0721 0.4545 0.3327
4.250 0.8959 0.01173 0.00545 -0.0718 0.4517 0.3502
4.500 0.9196 0.01187 0.00565 -0.0713 0.4482 0.3714
4.750 0.9441 0.01203 0.00590 -0.0711 0.4442 0.4072
5.000 1.2150 0.01159 0.00673 -0.1242 0.4327 1.0000
5.250 1.2338 0.01181 0.00694 -0.1227 0.4294 1.0000
5.500 1.2512 0.01208 0.00720 -0.1209 0.4256 1.0000
5.750 1.2661 0.01244 0.00752 -0.1188 0.4211 1.0000
6.000 1.2852 0.01269 0.00777 -0.1174 0.4183 1.0000
6.250 1.3053 0.01291 0.00801 -0.1162 0.4152 1.0000
6.500 1.3238 0.01319 0.00829 -0.1148 0.4113 1.0000
6.750 1.3391 0.01358 0.00866 -0.1129 0.4067 1.0000
7.000 1.3534 0.01403 0.00908 -0.1109 0.4018 1.0000
7.250 1.3732 0.01430 0.00938 -0.1098 0.3984 1.0000
7.500 1.3906 0.01467 0.00974 -0.1083 0.3936 1.0000
7.750 1.4052 0.01515 0.01021 -0.1065 0.3884 1.0000
8.000 1.4194 0.01568 0.01072 -0.1046 0.3836 1.0000
8.250 1.4379 0.01604 0.01110 -0.1035 0.3792 1.0000
8.500 1.4539 0.01653 0.01159 -0.1020 0.3747 1.0000
8.750 1.4665 0.01717 0.01222 -0.1001 0.3694 1.0000
9.000 1.4827 0.01769 0.01274 -0.0987 0.3650 1.0000
9.250 1.4982 0.01824 0.01331 -0.0973 0.3593 1.0000
9.500 1.5116 0.01891 0.01397 -0.0957 0.3541 1.0000
9.750 1.5242 0.01965 0.01470 -0.0940 0.3489 1.0000
10.000 1.5393 0.02027 0.01533 -0.0927 0.3424 1.0000
10.250 1.5503 0.02113 0.01618 -0.0909 0.3362 1.0000
10.500 1.5632 0.02191 0.01696 -0.0894 0.3302 1.0000
10.750 1.5759 0.02271 0.01776 -0.0879 0.3234 1.0000
11.000 1.5837 0.02382 0.01885 -0.0860 0.3158 1.0000
11.250 1.5955 0.02470 0.01973 -0.0845 0.3077 1.0000
11.500 1.6016 0.02597 0.02097 -0.0825 0.2990 1.0000
11.750 1.6094 0.02716 0.02214 -0.0807 0.2885 1.0000
12.000 1.6141 0.02859 0.02354 -0.0787 0.2775 1.0000
12.250 1.6145 0.03032 0.02521 -0.0764 0.2632 1.0000
12.500 1.6128 0.03225 0.02707 -0.0740 0.2476 1.0000
12.750 1.6089 0.03442 0.02918 -0.0715 0.2318 1.0000
13.000 1.6045 0.03667 0.03136 -0.0692 0.2165 1.0000
13.250 1.6002 0.03898 0.03363 -0.0669 0.2035 1.0000
13.500 1.5976 0.04125 0.03586 -0.0650 0.1939 1.0000
13.750 1.5996 0.04318 0.03779 -0.0634 0.1867 1.0000
14.000 1.5976 0.04551 0.04012 -0.0618 0.1804 1.0000
14.250 1.6013 0.04736 0.04199 -0.0605 0.1759 1.0000
14.500 1.6043 0.04936 0.04402 -0.0593 0.1727 1.0000
14.750 1.6068 0.05139 0.04607 -0.0582 0.1693 1.0000
15.000 1.6042 0.05398 0.04868 -0.0569 0.1650 1.0000
15.250 1.6095 0.05582 0.05057 -0.0560 0.1625 1.0000
15.500 1.6123 0.05795 0.05275 -0.0551 0.1598 1.0000
15.750 1.6146 0.06014 0.05498 -0.0543 0.1572 1.0000
16.000 1.6140 0.06268 0.05755 -0.0534 0.1547 1.0000
16.250 1.6084 0.06578 0.06068 -0.0524 0.1506 1.0000
16.500 1.6142 0.06767 0.06263 -0.0519 0.1490 1.0000
16.750 1.6166 0.06997 0.06498 -0.0513 0.1460 1.0000
17.000 1.6167 0.07250 0.06755 -0.0507 0.1427 1.0000
17.250 1.6092 0.07594 0.07101 -0.0501 0.1382 1.0000
17.500 1.6120 0.07823 0.07335 -0.0497 0.1346 1.0000
17.750 1.6090 0.08120 0.07635 -0.0493 0.1295 1.0000
18.000 1.6018 0.08466 0.07981 -0.0488 0.1228 1.0000
18.250 1.5939 0.08821 0.08335 -0.0484 0.1146 1.0000
18.500 1.5816 0.09237 0.08748 -0.0482 0.1048 1.0000
18.750 1.5739 0.09599 0.09110 -0.0480 0.0989 1.0000
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