St. CYR 24 (Bartel 35-IIIC) (stcyr24-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: St. CYR 24 (Bartel 35-IIIC) (stcyr24-il) Reynolds number: 1,000,000 Max Cl/Cd: 126.89 at α=1.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-stcyr24-il-1000000.txt Download as CSV file: xf-stcyr24-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: St. CYR 24 (Bartel 35-IIIC)
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
------ -------- --------- --------- -------- -------- --------
-13.750 0.0202 0.10084 0.09871 -0.1047 0.9086 0.0271
-13.500 0.0054 0.09440 0.09220 -0.1088 0.8993 0.0280
-13.250 0.0147 0.09117 0.08893 -0.1094 0.8908 0.0282
-13.000 0.0273 0.08915 0.08687 -0.1096 0.8836 0.0284
-12.750 0.0372 0.08692 0.08461 -0.1101 0.8769 0.0286
-12.500 0.0461 0.08461 0.08225 -0.1107 0.8707 0.0288
-12.250 0.0548 0.08234 0.07998 -0.1112 0.8660 0.0292
-12.000 0.0614 0.07969 0.07731 -0.1119 0.8613 0.0296
-11.750 -0.3432 0.02756 0.02434 -0.1535 0.8471 0.0287
-11.500 -0.3400 0.02480 0.02132 -0.1526 0.8425 0.0288
-11.250 -0.3246 0.02347 0.01983 -0.1518 0.8387 0.0290
-11.000 -0.3085 0.02209 0.01826 -0.1510 0.8348 0.0292
-10.750 -0.2894 0.02103 0.01707 -0.1502 0.8317 0.0295
-10.500 -0.2698 0.01999 0.01591 -0.1494 0.8288 0.0297
-10.250 -0.2478 0.01926 0.01508 -0.1487 0.8260 0.0301
-10.000 -0.2271 0.01823 0.01389 -0.1479 0.8233 0.0304
-9.750 -0.2060 0.01717 0.01264 -0.1471 0.8206 0.0307
-9.500 -0.1835 0.01629 0.01159 -0.1464 0.8178 0.0310
-9.250 -0.1597 0.01555 0.01068 -0.1458 0.8145 0.0312
-9.000 -0.1357 0.01487 0.00989 -0.1452 0.8125 0.0315
-8.750 -0.1108 0.01432 0.00924 -0.1446 0.8104 0.0317
-8.500 -0.0850 0.01391 0.00874 -0.1441 0.8079 0.0319
-8.250 -0.0624 0.01281 0.00750 -0.1433 0.8048 0.0324
-8.000 -0.0372 0.01229 0.00692 -0.1427 0.8014 0.0328
-7.750 -0.0106 0.01199 0.00656 -0.1423 0.7973 0.0332
-7.500 0.0157 0.01168 0.00622 -0.1418 0.7942 0.0336
-7.250 0.0421 0.01137 0.00589 -0.1413 0.7911 0.0341
-7.000 0.0688 0.01107 0.00555 -0.1409 0.7880 0.0345
-6.750 0.0958 0.01082 0.00526 -0.1405 0.7852 0.0351
-6.500 0.1230 0.01059 0.00497 -0.1402 0.7824 0.0357
-6.250 0.1506 0.01039 0.00471 -0.1399 0.7793 0.0360
-6.000 0.1767 0.00996 0.00424 -0.1394 0.7765 0.0367
-5.750 0.2033 0.00966 0.00395 -0.1390 0.7739 0.0374
-5.500 0.2304 0.00946 0.00376 -0.1386 0.7709 0.0381
-5.250 0.2578 0.00928 0.00356 -0.1383 0.7678 0.0389
-5.000 0.2852 0.00911 0.00337 -0.1380 0.7646 0.0398
-4.750 0.3130 0.00901 0.00321 -0.1377 0.7602 0.0406
-4.500 0.3392 0.00873 0.00294 -0.1372 0.7563 0.0417
-4.250 0.3661 0.00856 0.00279 -0.1368 0.7515 0.0431
-4.000 0.3934 0.00844 0.00266 -0.1364 0.7469 0.0446
-3.750 0.4211 0.00839 0.00256 -0.1361 0.7421 0.0460
-3.500 0.4474 0.00816 0.00237 -0.1356 0.7373 0.0483
-3.250 0.4746 0.00805 0.00227 -0.1353 0.7321 0.0505
-3.000 0.5015 0.00794 0.00213 -0.1349 0.7269 0.0533
-2.750 0.5286 0.00785 0.00206 -0.1346 0.7218 0.0566
-2.500 0.5554 0.00774 0.00197 -0.1342 0.7148 0.0605
-2.250 0.5817 0.00770 0.00190 -0.1336 0.7070 0.0648
-2.000 0.6083 0.00761 0.00185 -0.1332 0.6979 0.0706
-1.750 0.6340 0.00757 0.00179 -0.1326 0.6872 0.0767
-1.500 0.6593 0.00757 0.00176 -0.1319 0.6739 0.0829
-1.250 0.6848 0.00754 0.00174 -0.1313 0.6603 0.0919
-1.000 0.7097 0.00754 0.00173 -0.1305 0.6456 0.1010
-0.750 0.7336 0.00759 0.00172 -0.1296 0.6275 0.1107
-0.500 0.7560 0.00765 0.00174 -0.1284 0.6061 0.1264
-0.250 0.7775 0.00767 0.00185 -0.1271 0.5826 0.1935
0.000 0.7988 0.00783 0.00195 -0.1258 0.5585 0.2204
0.500 0.8415 0.00813 0.00218 -0.1231 0.5182 0.2678
1.000 0.8740 0.00740 0.00257 -0.1188 0.4873 0.7663
1.250 0.9377 0.00739 0.00286 -0.1268 0.4652 1.0000
1.500 0.9582 0.00759 0.00297 -0.1252 0.4497 1.0000
1.750 0.9783 0.00780 0.00309 -0.1237 0.4340 1.0000
2.000 0.9980 0.00802 0.00323 -0.1221 0.4180 1.0000
2.250 1.0171 0.00826 0.00337 -0.1203 0.4012 1.0000
2.500 1.0357 0.00852 0.00354 -0.1185 0.3837 1.0000
2.750 1.0529 0.00880 0.00372 -0.1164 0.3645 1.0000
3.000 1.0673 0.00911 0.00391 -0.1138 0.3450 1.0000
3.250 1.0809 0.00945 0.00413 -0.1111 0.3246 1.0000
3.500 1.0952 0.00979 0.00437 -0.1085 0.3038 1.0000
3.750 1.1093 0.01018 0.00464 -0.1060 0.2819 1.0000
4.000 1.1227 0.01062 0.00494 -0.1034 0.2601 1.0000
4.250 1.1370 0.01106 0.00527 -0.1011 0.2406 1.0000
4.500 1.1520 0.01149 0.00560 -0.0989 0.2244 1.0000
4.750 1.1682 0.01189 0.00592 -0.0970 0.2123 1.0000
5.000 1.1855 0.01225 0.00623 -0.0953 0.2035 1.0000
5.250 1.2025 0.01264 0.00658 -0.0937 0.1966 1.0000
5.500 1.2208 0.01298 0.00690 -0.0922 0.1918 1.0000
5.750 1.2395 0.01332 0.00722 -0.0909 0.1881 1.0000
6.000 1.2578 0.01368 0.00757 -0.0896 0.1850 1.0000
6.250 1.2751 0.01410 0.00797 -0.0881 0.1818 1.0000
6.500 1.2917 0.01456 0.00843 -0.0866 0.1784 1.0000
6.750 1.3113 0.01489 0.00878 -0.0855 0.1773 1.0000
7.000 1.3305 0.01525 0.00916 -0.0845 0.1759 1.0000
7.250 1.3493 0.01563 0.00956 -0.0834 0.1743 1.0000
7.500 1.3674 0.01606 0.01001 -0.0823 0.1730 1.0000
7.750 1.3852 0.01652 0.01048 -0.0811 0.1713 1.0000
8.000 1.4023 0.01702 0.01099 -0.0799 0.1695 1.0000
8.250 1.4182 0.01760 0.01157 -0.0786 0.1672 1.0000
8.500 1.4316 0.01833 0.01230 -0.0771 0.1636 1.0000
8.750 1.4511 0.01874 0.01275 -0.0763 0.1627 1.0000
9.000 1.4699 0.01919 0.01323 -0.0755 0.1615 1.0000
9.250 1.4881 0.01967 0.01376 -0.0747 0.1603 1.0000
9.500 1.5057 0.02020 0.01431 -0.0738 0.1585 1.0000
9.750 1.5227 0.02078 0.01491 -0.0729 0.1569 1.0000
10.000 1.5383 0.02144 0.01558 -0.0719 0.1545 1.0000
10.250 1.5526 0.02221 0.01636 -0.0707 0.1523 1.0000
10.500 1.5641 0.02315 0.01731 -0.0693 0.1495 1.0000
10.750 1.5829 0.02363 0.01786 -0.0687 0.1484 1.0000
11.000 1.6010 0.02416 0.01844 -0.0681 0.1469 1.0000
11.250 1.6182 0.02476 0.01908 -0.0674 0.1451 1.0000
11.500 1.6340 0.02547 0.01981 -0.0666 0.1425 1.0000
11.750 1.6482 0.02628 0.02064 -0.0657 0.1401 1.0000
12.000 1.6593 0.02732 0.02168 -0.0645 0.1366 1.0000
12.250 1.6753 0.02803 0.02245 -0.0639 0.1349 1.0000
12.500 1.6920 0.02870 0.02316 -0.0633 0.1319 1.0000
12.750 1.7062 0.02956 0.02403 -0.0625 0.1281 1.0000
13.000 1.7163 0.03073 0.02520 -0.0615 0.1237 1.0000
13.250 1.7307 0.03158 0.02609 -0.0608 0.1189 1.0000
13.500 1.7395 0.03288 0.02735 -0.0597 0.1106 1.0000
13.750 1.7440 0.03453 0.02894 -0.0584 0.0986 1.0000
14.000 1.7444 0.03657 0.03093 -0.0569 0.0888 1.0000
14.250 1.7445 0.03869 0.03301 -0.0554 0.0820 1.0000
14.500 1.7474 0.04062 0.03497 -0.0542 0.0775 1.0000
14.750 1.7477 0.04284 0.03721 -0.0531 0.0733 1.0000
15.000 1.7527 0.04469 0.03911 -0.0522 0.0699 1.0000
15.250 1.7504 0.04726 0.04169 -0.0512 0.0651 1.0000
15.500 1.7536 0.04937 0.04385 -0.0505 0.0614 1.0000
15.750 1.7510 0.05210 0.04659 -0.0497 0.0563 1.0000
16.000 1.7478 0.05497 0.04948 -0.0490 0.0514 1.0000
16.250 1.7442 0.05796 0.05249 -0.0485 0.0468 1.0000
16.500 1.7383 0.06127 0.05583 -0.0480 0.0431 1.0000
16.750 1.7314 0.06481 0.05942 -0.0478 0.0402 1.0000
17.000 1.7264 0.06825 0.06291 -0.0477 0.0384 1.0000
17.250 1.7194 0.07197 0.06670 -0.0478 0.0366 1.0000
17.500 1.7096 0.07613 0.07093 -0.0481 0.0351 1.0000
17.750 1.7022 0.08010 0.07499 -0.0486 0.0339 1.0000
18.000 1.6947 0.08417 0.07915 -0.0492 0.0330 1.0000
18.250 1.6846 0.08868 0.08375 -0.0501 0.0320 1.0000
18.500 1.6721 0.09360 0.08876 -0.0511 0.0312 1.0000
18.750 1.6559 0.09922 0.09448 -0.0526 0.0304 1.0000
|
Polar data table (+)
Polar graphs
<< Back to St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)