SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: SARATOV AIRFOIL (saratov-il) Reynolds number: 1,000,000 Max Cl/Cd: 136.85 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-saratov-il-1000000-n5.txt Download as CSV file: xf-saratov-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: SARATOV 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
------ -------- --------- --------- -------- -------- --------
-10.750 -0.3009 0.06103 0.05713 -0.1149 0.5128 0.0257
-10.500 -0.3111 0.05506 0.05107 -0.1214 0.5120 0.0261
-10.250 -0.3062 0.05058 0.04651 -0.1271 0.5106 0.0264
-9.750 -0.2755 0.04377 0.03954 -0.1371 0.5080 0.0274
-9.500 -0.2539 0.04131 0.03704 -0.1410 0.5070 0.0281
-9.250 -0.2306 0.03922 0.03492 -0.1442 0.5059 0.0287
-9.000 -0.2061 0.03676 0.03238 -0.1482 0.5048 0.0293
-8.750 -0.1802 0.03455 0.03009 -0.1518 0.5035 0.0298
-8.500 -0.1533 0.03260 0.02804 -0.1551 0.5023 0.0304
-8.250 -0.1255 0.03065 0.02599 -0.1583 0.5009 0.0308
-8.000 -0.0971 0.02869 0.02391 -0.1615 0.4995 0.0313
-7.750 -0.0686 0.02715 0.02225 -0.1640 0.4981 0.0317
-7.500 -0.0400 0.02573 0.02072 -0.1662 0.4968 0.0320
-7.250 -0.0113 0.02435 0.01922 -0.1683 0.4955 0.0323
-7.000 0.0174 0.02311 0.01788 -0.1701 0.4943 0.0325
-6.750 0.0463 0.02202 0.01669 -0.1717 0.4930 0.0332
-6.500 0.0753 0.02086 0.01543 -0.1733 0.4917 0.0342
-6.250 0.1043 0.01963 0.01412 -0.1749 0.4913 0.0348
-6.000 0.1332 0.01856 0.01297 -0.1762 0.4907 0.0355
-5.750 0.1619 0.01753 0.01184 -0.1774 0.4902 0.0362
-5.500 0.1905 0.01661 0.01082 -0.1783 0.4896 0.0368
-5.250 0.2190 0.01577 0.00989 -0.1792 0.4889 0.0376
-5.000 0.2475 0.01502 0.00905 -0.1799 0.4883 0.0383
-4.750 0.2759 0.01436 0.00829 -0.1804 0.4876 0.0389
-4.500 0.3042 0.01379 0.00763 -0.1809 0.4869 0.0395
-4.250 0.3324 0.01332 0.00709 -0.1812 0.4862 0.0399
-4.000 0.3608 0.01271 0.00638 -0.1817 0.4855 0.0410
-3.750 0.3891 0.01211 0.00568 -0.1822 0.4848 0.0428
-3.500 0.4172 0.01169 0.00520 -0.1824 0.4841 0.0445
-3.250 0.4452 0.01137 0.00482 -0.1825 0.4835 0.0459
-3.000 0.4732 0.01112 0.00452 -0.1826 0.4828 0.0473
-2.750 0.5012 0.01093 0.00427 -0.1826 0.4821 0.0484
-2.500 0.5290 0.01076 0.00405 -0.1826 0.4815 0.0494
-2.250 0.5569 0.01061 0.00387 -0.1825 0.4809 0.0501
-2.000 0.5848 0.01042 0.00362 -0.1825 0.4803 0.0532
-1.750 0.6125 0.01025 0.00342 -0.1825 0.4796 0.0569
-1.500 0.6403 0.01009 0.00325 -0.1824 0.4790 0.0611
-1.250 0.6679 0.00991 0.00307 -0.1823 0.4784 0.0739
-1.000 0.6952 0.00960 0.00288 -0.1824 0.4777 0.1183
-0.750 0.7228 0.00960 0.00287 -0.1822 0.4771 0.1249
-0.500 0.7503 0.00961 0.00288 -0.1820 0.4764 0.1280
-0.250 0.7776 0.00962 0.00290 -0.1818 0.4751 0.1325
0.000 0.8055 0.00959 0.00289 -0.1817 0.4744 0.1362
0.250 0.8333 0.00957 0.00288 -0.1816 0.4733 0.1378
0.500 0.8609 0.00957 0.00288 -0.1814 0.4726 0.1390
0.750 0.8885 0.00958 0.00290 -0.1813 0.4721 0.1398
1.000 0.9161 0.00958 0.00291 -0.1811 0.4711 0.1412
1.250 0.9436 0.00957 0.00292 -0.1809 0.4700 0.1440
1.500 0.9710 0.00958 0.00295 -0.1808 0.4691 0.1455
1.750 0.9984 0.00959 0.00299 -0.1806 0.4682 0.1470
2.000 1.0257 0.00960 0.00302 -0.1804 0.4668 0.1489
2.250 1.0529 0.00962 0.00306 -0.1802 0.4657 0.1511
2.500 1.0800 0.00965 0.00310 -0.1800 0.4640 0.1523
2.750 1.1070 0.00969 0.00314 -0.1797 0.4622 0.1533
3.000 1.1338 0.00974 0.00320 -0.1795 0.4608 0.1541
3.250 1.1604 0.00981 0.00328 -0.1792 0.4592 0.1548
3.500 1.1876 0.00983 0.00334 -0.1790 0.4584 0.1554
3.750 1.2148 0.00984 0.00340 -0.1788 0.4571 0.1573
4.000 1.2419 0.00984 0.00346 -0.1786 0.4550 0.1596
4.250 1.2688 0.00986 0.00352 -0.1784 0.4522 0.1618
4.500 1.2954 0.00989 0.00359 -0.1781 0.4495 0.1639
4.750 1.3217 0.00994 0.00367 -0.1778 0.4465 0.1661
5.000 1.3479 0.00999 0.00375 -0.1775 0.4419 0.1684
5.250 1.3740 0.01004 0.00381 -0.1771 0.4311 0.1707
5.500 1.3820 0.01147 0.00460 -0.1739 0.3128 0.1719
5.750 1.3772 0.01381 0.00620 -0.1686 0.1693 0.1739
6.000 1.3967 0.01424 0.00660 -0.1672 0.1541 0.1781
6.250 1.4172 0.01456 0.00692 -0.1659 0.1459 0.1820
6.500 1.4378 0.01487 0.00724 -0.1647 0.1388 0.1861
6.750 1.4579 0.01517 0.00755 -0.1634 0.1322 0.1907
7.000 1.4763 0.01553 0.00792 -0.1618 0.1244 0.1978
7.500 1.5063 0.01626 0.00866 -0.1573 0.1060 0.2168
7.750 1.5175 0.01676 0.00915 -0.1545 0.0940 0.2380
8.000 1.5259 0.01744 0.00983 -0.1512 0.0787 0.2680
8.250 1.5291 0.01840 0.01073 -0.1473 0.0603 0.2815
8.500 1.5294 0.01954 0.01181 -0.1432 0.0432 0.2883
8.750 1.5274 0.02085 0.01307 -0.1391 0.0288 0.2935
9.000 1.5287 0.02216 0.01438 -0.1356 0.0206 0.2965
9.250 1.5337 0.02337 0.01561 -0.1329 0.0172 0.3004
9.500 1.5386 0.02465 0.01692 -0.1303 0.0153 0.3044
9.750 1.5448 0.02592 0.01824 -0.1281 0.0141 0.3075
10.000 1.5510 0.02734 0.01971 -0.1261 0.0135 0.3087
10.250 1.5559 0.02896 0.02140 -0.1242 0.0128 0.3098
10.500 1.5592 0.03083 0.02333 -0.1223 0.0120 0.3109
10.750 1.5622 0.03285 0.02540 -0.1207 0.0114 0.3122
11.000 1.5649 0.03503 0.02764 -0.1192 0.0108 0.3135
11.250 1.5700 0.03705 0.02973 -0.1180 0.0105 0.3153
11.500 1.5743 0.03921 0.03195 -0.1169 0.0101 0.3168
11.750 1.5785 0.04143 0.03422 -0.1159 0.0097 0.3187
12.000 1.5822 0.04375 0.03660 -0.1149 0.0093 0.3199
12.250 1.5857 0.04615 0.03905 -0.1140 0.0090 0.3208
12.500 1.5886 0.04864 0.04160 -0.1131 0.0086 0.3216
12.750 1.5918 0.05113 0.04415 -0.1123 0.0083 0.3222
13.000 1.5945 0.05371 0.04679 -0.1116 0.0080 0.3227
13.250 1.6001 0.05595 0.04909 -0.1109 0.0078 0.3236
13.500 1.6052 0.05830 0.05150 -0.1103 0.0077 0.3246
13.750 1.6109 0.06059 0.05385 -0.1097 0.0075 0.3260
14.000 1.6165 0.06292 0.05625 -0.1092 0.0073 0.3279
14.250 1.6228 0.06513 0.05851 -0.1087 0.0070 0.3283
14.500 1.6285 0.06748 0.06090 -0.1083 0.0068 0.3293
14.750 1.6347 0.06975 0.06323 -0.1079 0.0066 0.3300
15.000 1.6412 0.07201 0.06553 -0.1075 0.0064 0.3308
15.250 1.6463 0.07449 0.06805 -0.1072 0.0061 0.3318
15.500 1.6509 0.07704 0.07065 -0.1069 0.0059 0.3323
15.750 1.6564 0.07949 0.07316 -0.1067 0.0057 0.3326
16.000 1.6630 0.08182 0.07557 -0.1065 0.0057 0.3329
16.250 1.6684 0.08435 0.07817 -0.1064 0.0056 0.3331
16.500 1.6744 0.08682 0.08070 -0.1062 0.0055 0.3334
16.750 1.6806 0.08922 0.08316 -0.1062 0.0053 0.3337
17.000 1.6859 0.09178 0.08580 -0.1061 0.0052 0.3340
17.250 1.6905 0.09450 0.08859 -0.1062 0.0051 0.3343
17.500 1.6955 0.09714 0.09130 -0.1063 0.0050 0.3346
17.750 1.7009 0.09973 0.09395 -0.1064 0.0049 0.3349
18.000 1.7053 0.10250 0.09680 -0.1066 0.0048 0.3353
18.250 1.7088 0.10542 0.09979 -0.1069 0.0047 0.3356
18.500 1.7126 0.10828 0.10272 -0.1072 0.0046 0.3360
18.750 1.7162 0.11116 0.10567 -0.1076 0.0045 0.3364
19.000 1.7179 0.11440 0.10899 -0.1081 0.0044 0.3367
19.250 1.7195 0.11766 0.11232 -0.1087 0.0043 0.3371
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