SARATOV AIRFOIL (saratov-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: SARATOV AIRFOIL (saratov-il) Reynolds number: 1,000,000 Max Cl/Cd: 145.9 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-saratov-il-1000000.txt Download as CSV file: xf-saratov-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.000 -0.0209 0.09268 0.08876 -0.1020 0.5313 0.0260
-9.750 -0.0254 0.08762 0.08372 -0.1042 0.5307 0.0266
-9.500 -0.0030 0.08842 0.08450 -0.1036 0.5289 0.0279
-9.250 0.0086 0.08684 0.08292 -0.1042 0.5274 0.0287
-9.000 0.0077 0.08320 0.07930 -0.1064 0.5264 0.0319
-8.750 0.0126 0.08032 0.07642 -0.1074 0.5254 0.0319
-8.250 -0.1264 0.03163 0.02729 -0.1568 0.5280 0.0333
-8.000 -0.0985 0.02980 0.02539 -0.1599 0.5263 0.0340
-7.750 -0.0701 0.02800 0.02351 -0.1629 0.5246 0.0347
-7.500 -0.0408 0.02591 0.02129 -0.1664 0.5229 0.0354
-7.250 -0.0113 0.02395 0.01917 -0.1694 0.5211 0.0361
-7.000 0.0179 0.02228 0.01735 -0.1719 0.5193 0.0368
-6.750 0.0468 0.02090 0.01581 -0.1739 0.5173 0.0374
-6.500 0.0756 0.01974 0.01453 -0.1754 0.5161 0.0380
-6.250 0.1047 0.01871 0.01339 -0.1767 0.5153 0.0384
-6.000 0.1334 0.01768 0.01223 -0.1778 0.5144 0.0395
-5.750 0.1620 0.01697 0.01145 -0.1786 0.5135 0.0406
-5.500 0.1906 0.01625 0.01066 -0.1793 0.5124 0.0415
-5.250 0.2191 0.01561 0.00995 -0.1799 0.5114 0.0424
-5.000 0.2475 0.01500 0.00925 -0.1805 0.5104 0.0434
-4.750 0.2759 0.01446 0.00863 -0.1810 0.5095 0.0444
-4.500 0.3042 0.01397 0.00805 -0.1813 0.5085 0.0454
-4.250 0.3325 0.01358 0.00758 -0.1816 0.5076 0.0461
-4.000 0.3609 0.01308 0.00698 -0.1820 0.5067 0.0475
-3.750 0.3893 0.01249 0.00630 -0.1824 0.5058 0.0497
-3.500 0.4174 0.01207 0.00580 -0.1826 0.5049 0.0514
-3.250 0.4454 0.01173 0.00538 -0.1828 0.5040 0.0531
-3.000 0.4734 0.01147 0.00504 -0.1829 0.5030 0.0547
-2.750 0.5012 0.01128 0.00479 -0.1829 0.5019 0.0562
-2.500 0.5291 0.01091 0.00433 -0.1830 0.5008 0.0609
-2.250 0.5569 0.01069 0.00406 -0.1831 0.4998 0.0649
-2.000 0.5849 0.01034 0.00370 -0.1831 0.4995 0.0770
-1.750 0.6125 0.00995 0.00345 -0.1833 0.4992 0.1259
-1.500 0.6404 0.00993 0.00346 -0.1832 0.4988 0.1335
-1.250 0.6683 0.00998 0.00351 -0.1830 0.4984 0.1382
-1.000 0.6963 0.01005 0.00357 -0.1829 0.4980 0.1401
-0.750 0.7241 0.01002 0.00354 -0.1828 0.4976 0.1434
-0.500 0.7519 0.01006 0.00360 -0.1827 0.4972 0.1462
-0.250 0.7797 0.01013 0.00368 -0.1825 0.4967 0.1487
0.000 0.8074 0.01015 0.00370 -0.1824 0.4957 0.1507
0.250 0.8351 0.01014 0.00369 -0.1822 0.4943 0.1522
0.500 0.8627 0.01014 0.00368 -0.1820 0.4931 0.1534
0.750 0.8904 0.01019 0.00373 -0.1819 0.4924 0.1544
1.000 0.9179 0.01016 0.00370 -0.1817 0.4915 0.1567
1.250 0.9453 0.01013 0.00368 -0.1816 0.4905 0.1592
1.500 0.9728 0.01014 0.00370 -0.1814 0.4895 0.1606
1.750 1.0002 0.01018 0.00375 -0.1812 0.4888 0.1625
2.000 1.0275 0.01021 0.00380 -0.1811 0.4877 0.1642
2.250 1.0548 0.01027 0.00386 -0.1809 0.4863 0.1653
2.500 1.0820 0.01039 0.00397 -0.1807 0.4846 0.1666
2.750 1.1093 0.01046 0.00406 -0.1806 0.4833 0.1677
3.000 1.1365 0.01045 0.00408 -0.1804 0.4827 0.1689
3.250 1.1637 0.01045 0.00412 -0.1802 0.4820 0.1698
3.500 1.1908 0.01045 0.00415 -0.1799 0.4811 0.1710
3.750 1.2178 0.01041 0.00416 -0.1797 0.4799 0.1741
4.000 1.2446 0.01038 0.00419 -0.1795 0.4783 0.1767
4.250 1.2714 0.01038 0.00423 -0.1792 0.4767 0.1791
4.500 1.2982 0.01039 0.00428 -0.1789 0.4751 0.1815
4.750 1.3248 0.01040 0.00433 -0.1786 0.4735 0.1840
5.000 1.3506 0.01042 0.00435 -0.1782 0.4699 0.1860
5.250 1.3766 0.01040 0.00439 -0.1778 0.4660 0.1917
5.500 1.4029 0.01028 0.00436 -0.1775 0.4617 0.1972
5.750 1.4290 0.01025 0.00436 -0.1771 0.4570 0.2019
6.000 1.4543 0.01025 0.00442 -0.1766 0.4509 0.2120
6.250 1.4800 0.01020 0.00443 -0.1761 0.4396 0.2284
6.500 1.5042 0.01031 0.00460 -0.1755 0.4150 0.2704
6.750 1.4786 0.01394 0.00694 -0.1667 0.1895 0.2761
7.000 1.4908 0.01478 0.00765 -0.1641 0.1618 0.2925
7.250 1.5074 0.01535 0.00820 -0.1621 0.1494 0.2984
7.500 1.5213 0.01582 0.00863 -0.1597 0.1390 0.3061
7.750 1.5358 0.01624 0.00907 -0.1573 0.1319 0.3080
8.000 1.5483 0.01678 0.00960 -0.1546 0.1240 0.3097
8.250 1.5624 0.01727 0.01010 -0.1523 0.1167 0.3115
8.500 1.5736 0.01787 0.01068 -0.1496 0.1074 0.3138
8.750 1.5812 0.01863 0.01139 -0.1464 0.0933 0.3173
9.000 1.5795 0.01985 0.01246 -0.1421 0.0701 0.3204
9.250 1.5696 0.02161 0.01410 -0.1370 0.0450 0.3210
9.500 1.5586 0.02367 0.01609 -0.1322 0.0282 0.3215
9.750 1.5569 0.02541 0.01784 -0.1290 0.0226 0.3223
10.000 1.5594 0.02702 0.01951 -0.1265 0.0204 0.3231
10.250 1.5601 0.02891 0.02144 -0.1241 0.0188 0.3240
10.500 1.5600 0.03104 0.02364 -0.1219 0.0176 0.3250
10.750 1.5638 0.03297 0.02565 -0.1203 0.0170 0.3263
11.000 1.5664 0.03513 0.02788 -0.1188 0.0163 0.3276
11.250 1.5687 0.03741 0.03023 -0.1175 0.0158 0.3293
11.500 1.5694 0.03994 0.03282 -0.1162 0.0152 0.3312
11.750 1.5687 0.04271 0.03564 -0.1150 0.0146 0.3331
12.000 1.5643 0.04594 0.03896 -0.1137 0.0139 0.3347
12.250 1.5697 0.04812 0.04121 -0.1129 0.0137 0.3355
12.500 1.5745 0.05042 0.04358 -0.1121 0.0133 0.3370
12.750 1.5783 0.05286 0.04609 -0.1114 0.0130 0.3384
13.000 1.5820 0.05532 0.04861 -0.1107 0.0126 0.3396
13.250 1.5859 0.05777 0.05111 -0.1100 0.0123 0.3412
13.500 1.5897 0.06028 0.05367 -0.1094 0.0119 0.3437
13.750 1.5926 0.06292 0.05636 -0.1087 0.0116 0.3468
14.000 1.5939 0.06578 0.05929 -0.1082 0.0113 0.3492
14.250 1.5893 0.06940 0.06300 -0.1076 0.0109 0.3508
14.500 1.5956 0.07172 0.06539 -0.1072 0.0107 0.3527
14.750 1.6020 0.07406 0.06779 -0.1069 0.0106 0.3535
15.000 1.6085 0.07636 0.07015 -0.1065 0.0104 0.3541
15.250 1.6140 0.07883 0.07270 -0.1063 0.0102 0.3550
15.500 1.6193 0.08137 0.07529 -0.1061 0.0099 0.3561
15.750 1.6254 0.08381 0.07779 -0.1059 0.0097 0.3571
16.000 1.6313 0.08626 0.08030 -0.1057 0.0094 0.3577
16.250 1.6363 0.08891 0.08300 -0.1057 0.0092 0.3582
16.500 1.6412 0.09156 0.08571 -0.1057 0.0090 0.3587
16.750 1.6447 0.09441 0.08860 -0.1057 0.0088 0.3592
17.000 1.6447 0.09779 0.09204 -0.1058 0.0085 0.3596
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