TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il) Reynolds number: 200,000 Max Cl/Cd: 56.12 at α=7.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-tsagi-r-3a-il-200000.txt Download as CSV file: xf-tsagi-r-3a-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: TsAGI R-3a (12%)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.250 -0.3306 0.09865 0.09559 -0.0010 1.0045 0.0547
-9.000 -0.3374 0.09397 0.09094 -0.0042 1.0045 0.0566
-8.750 -0.3679 0.08673 0.08374 -0.0134 1.0045 0.0574
-8.500 -0.3508 0.08354 0.08060 -0.0103 1.0045 0.0580
-8.250 -0.3381 0.08084 0.07793 -0.0089 1.0045 0.0589
-8.000 -0.3321 0.07752 0.07465 -0.0093 1.0045 0.0600
-7.750 -0.3310 0.07362 0.07079 -0.0108 1.0045 0.0613
-7.500 -0.3361 0.06892 0.06615 -0.0139 1.0045 0.0630
-7.250 -0.3836 0.05803 0.05505 -0.0294 1.0045 0.0653
-7.000 -0.3799 0.05285 0.04989 -0.0298 1.0045 0.0660
-6.750 -0.3653 0.05043 0.04759 -0.0284 1.0045 0.0669
-6.500 -0.3544 0.04767 0.04488 -0.0280 1.0045 0.0682
-6.250 -0.3527 0.03948 0.03613 -0.0348 0.9778 0.0751
-6.000 -0.3182 0.03553 0.03229 -0.0372 0.8991 0.0766
-5.750 -0.3471 0.04587 0.04229 -0.0341 0.9733 0.0770
-5.500 -0.3130 0.04199 0.03780 -0.0382 0.8861 0.0860
-5.250 -0.2965 0.02707 0.02114 -0.0367 0.8442 0.0433
-5.000 -0.2783 0.02511 0.01854 -0.0342 0.7499 0.0424
-4.750 -0.2565 0.02355 0.01628 -0.0325 0.6835 0.0428
-4.500 -0.2319 0.02220 0.01433 -0.0314 0.6413 0.0433
-4.250 -0.2058 0.02089 0.01258 -0.0306 0.6127 0.0434
-4.000 -0.1789 0.01981 0.01112 -0.0300 0.5917 0.0438
-3.750 -0.1519 0.01868 0.00978 -0.0294 0.5764 0.0447
-3.500 -0.1251 0.01787 0.00888 -0.0289 0.5644 0.0463
-3.250 -0.0977 0.01717 0.00810 -0.0285 0.5529 0.0486
-3.000 -0.0710 0.01649 0.00734 -0.0280 0.5436 0.0522
-2.750 -0.0437 0.01594 0.00677 -0.0276 0.5345 0.0581
-2.500 -0.0174 0.01534 0.00617 -0.0271 0.5272 0.0673
-2.250 0.0100 0.01487 0.00577 -0.0267 0.5191 0.0833
-2.000 0.0371 0.01453 0.00547 -0.0264 0.5117 0.1047
-1.750 0.0639 0.01406 0.00521 -0.0261 0.5045 0.1509
-1.500 0.0892 0.01328 0.00495 -0.0259 0.4974 0.2674
-1.250 0.1078 0.01202 0.00490 -0.0243 0.4918 0.5940
-1.000 0.1263 0.01137 0.00504 -0.0211 0.4852 0.8127
-0.750 0.1658 0.01137 0.00508 -0.0219 0.4773 0.9311
-0.500 0.2310 0.01154 0.00506 -0.0286 0.4674 0.9874
-0.250 0.2697 0.01163 0.00495 -0.0307 0.4592 0.9955
0.000 0.2947 0.01173 0.00492 -0.0302 0.4517 0.9955
0.250 0.3199 0.01182 0.00487 -0.0296 0.4435 0.9955
0.500 0.3451 0.01198 0.00488 -0.0290 0.4354 0.9955
0.750 0.3705 0.01209 0.00488 -0.0285 0.4262 0.9955
1.000 0.3959 0.01227 0.00494 -0.0279 0.4175 0.9955
1.250 0.4215 0.01241 0.00497 -0.0273 0.4080 0.9955
1.500 0.4472 0.01260 0.00506 -0.0268 0.3985 0.9955
1.750 0.4730 0.01275 0.00510 -0.0263 0.3892 0.9955
2.000 0.4990 0.01293 0.00523 -0.0258 0.3795 0.9955
2.250 0.5251 0.01310 0.00527 -0.0253 0.3713 0.9955
2.500 0.5515 0.01328 0.00542 -0.0249 0.3623 0.9955
2.750 0.5779 0.01343 0.00546 -0.0245 0.3551 0.9955
3.000 0.6044 0.01363 0.00562 -0.0242 0.3476 0.9955
3.250 0.6311 0.01380 0.00574 -0.0238 0.3411 0.9955
3.500 0.6576 0.01407 0.00588 -0.0235 0.3361 0.9955
3.750 0.6844 0.01427 0.00613 -0.0232 0.3297 0.9955
4.000 0.7110 0.01444 0.00622 -0.0229 0.3240 0.9955
4.250 0.7376 0.01468 0.00640 -0.0226 0.3184 0.9955
4.500 0.7642 0.01488 0.00661 -0.0223 0.3125 0.9955
4.750 0.7907 0.01510 0.00676 -0.0220 0.3078 0.9955
5.000 0.8172 0.01542 0.00705 -0.0217 0.3033 0.9955
5.250 0.8436 0.01570 0.00736 -0.0215 0.2985 0.9955
5.500 0.8700 0.01597 0.00759 -0.0212 0.2941 0.9955
5.750 0.8963 0.01639 0.00788 -0.0210 0.2901 0.9955
6.000 0.9224 0.01672 0.00833 -0.0207 0.2860 0.9955
6.250 0.9484 0.01705 0.00869 -0.0204 0.2817 0.9955
6.500 0.9745 0.01741 0.00899 -0.0202 0.2776 0.9955
6.750 1.0003 0.01794 0.00949 -0.0199 0.2735 0.9955
7.000 1.0256 0.01832 0.00998 -0.0196 0.2691 0.9955
7.250 1.0511 0.01873 0.01041 -0.0193 0.2649 0.9955
7.500 1.0768 0.01923 0.01084 -0.0191 0.2610 0.9955
7.750 1.1016 0.01984 0.01151 -0.0188 0.2569 0.9955
8.000 1.1258 0.02025 0.01206 -0.0183 0.2521 0.9955
8.250 1.1507 0.02068 0.01249 -0.0180 0.2475 0.9955
8.500 1.1761 0.02145 0.01314 -0.0179 0.2430 0.9955
8.750 1.1985 0.02185 0.01379 -0.0172 0.2384 0.9955
9.000 1.2222 0.02231 0.01433 -0.0168 0.2336 0.9955
9.250 1.2470 0.02285 0.01480 -0.0165 0.2295 0.9955
9.500 1.2692 0.02359 0.01566 -0.0159 0.2250 0.9955
9.750 1.2908 0.02412 0.01635 -0.0153 0.2202 0.9955
10.000 1.3143 0.02458 0.01680 -0.0148 0.2159 0.9955
10.250 1.3381 0.02540 0.01756 -0.0146 0.2119 0.9955
10.500 1.3565 0.02603 0.01847 -0.0136 0.2075 0.9955
10.750 1.3775 0.02664 0.01917 -0.0129 0.2035 0.9955
11.000 1.4004 0.02716 0.01968 -0.0124 0.2001 0.9955
11.250 1.4215 0.02806 0.02060 -0.0119 0.1966 0.9955
11.500 1.4370 0.02878 0.02159 -0.0107 0.1926 0.9955
11.750 1.4559 0.02922 0.02211 -0.0098 0.1886 0.9955
12.000 1.4778 0.02949 0.02231 -0.0092 0.1850 0.9955
12.250 1.4924 0.03033 0.02331 -0.0081 0.1813 0.9955
12.500 1.5053 0.03106 0.02424 -0.0067 0.1776 0.9955
12.750 1.5214 0.03154 0.02478 -0.0056 0.1742 0.9955
13.000 1.5400 0.03193 0.02511 -0.0047 0.1710 0.9955
13.250 1.5466 0.03299 0.02639 -0.0029 0.1678 0.9955
13.500 1.5497 0.03394 0.02751 -0.0006 0.1645 0.9955
13.750 1.5565 0.03481 0.02845 0.0011 0.1616 0.9955
14.000 1.5664 0.03565 0.02931 0.0022 0.1591 0.9955
14.250 1.5724 0.03701 0.03074 0.0034 0.1565 0.9955
14.500 1.5675 0.03917 0.03314 0.0043 0.1540 0.9955
14.750 1.5664 0.04130 0.03542 0.0045 0.1513 0.9955
15.000 1.5688 0.04324 0.03744 0.0045 0.1487 0.9955
15.250 1.5785 0.04455 0.03869 0.0047 0.1458 0.9955
15.500 1.5704 0.04794 0.04229 0.0038 0.1436 0.9955
15.750 1.5579 0.05212 0.04668 0.0023 0.1413 0.9955
16.000 1.5489 0.05603 0.05075 0.0007 0.1389 0.9955
16.250 1.5460 0.05919 0.05398 -0.0005 0.1365 0.9955
16.500 1.5591 0.06010 0.05479 0.0000 0.1335 0.9955
16.750 1.5380 0.06583 0.06075 -0.0025 0.1319 0.9955
17.000 1.5097 0.07274 0.06790 -0.0058 0.1302 0.9955
17.250 1.4801 0.08012 0.07548 -0.0093 0.1284 0.9955
17.500 1.4557 0.08695 0.08246 -0.0125 0.1264 0.9955
17.750 1.4754 0.08683 0.08227 -0.0120 0.1231 0.9955
18.000 1.4672 0.09113 0.08663 -0.0137 0.1207 0.9955
18.250 1.3921 0.10683 0.10264 -0.0218 0.1198 0.9955
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