FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 79-W-151 A (fx79w151a-il) Reynolds number: 200,000 Max Cl/Cd: 71.36 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx79w151a-il-200000-n5.txt Download as CSV file: xf-fx79w151a-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 79-W-151 A
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.000 -0.5562 0.08884 0.08507 -0.0571 1.0000 0.0177
-13.750 -0.6021 0.07667 0.07278 -0.0643 1.0000 0.0176
-13.500 -0.6312 0.06781 0.06382 -0.0699 1.0000 0.0174
-13.250 -0.6594 0.05879 0.05467 -0.0764 1.0000 0.0172
-13.000 -0.6842 0.05067 0.04637 -0.0831 1.0000 0.0172
-12.750 -0.7021 0.04510 0.04064 -0.0872 1.0000 0.0170
-12.500 -0.7190 0.04102 0.03637 -0.0890 1.0000 0.0173
-12.250 -0.7176 0.03727 0.03232 -0.0926 0.9725 0.0176
-12.000 -0.7071 0.03435 0.02917 -0.0955 0.9534 0.0180
-11.750 -0.6967 0.03231 0.02700 -0.0964 0.9359 0.0187
-11.500 -0.6883 0.03077 0.02527 -0.0956 0.9202 0.0193
-11.250 -0.6808 0.02955 0.02387 -0.0937 0.9063 0.0198
-11.000 -0.6742 0.02838 0.02252 -0.0915 0.8940 0.0206
-10.750 -0.6648 0.02725 0.02117 -0.0893 0.8835 0.0215
-10.500 -0.6538 0.02625 0.01996 -0.0872 0.8733 0.0223
-10.250 -0.6431 0.02528 0.01888 -0.0851 0.8638 0.0238
-10.000 -0.6287 0.02450 0.01796 -0.0834 0.8556 0.0252
-9.750 -0.6135 0.02371 0.01701 -0.0817 0.8466 0.0269
-9.500 -0.5963 0.02295 0.01602 -0.0801 0.8394 0.0288
-9.250 -0.5815 0.02208 0.01510 -0.0783 0.8307 0.0307
-9.000 -0.5629 0.02145 0.01432 -0.0770 0.8239 0.0331
-8.750 -0.5427 0.02088 0.01360 -0.0758 0.8157 0.0360
-8.500 -0.5243 0.02018 0.01283 -0.0744 0.8090 0.0389
-8.250 -0.5033 0.01969 0.01222 -0.0734 0.8013 0.0426
-8.000 -0.4821 0.01915 0.01155 -0.0723 0.7946 0.0463
-7.750 -0.4607 0.01868 0.01104 -0.0714 0.7873 0.0506
-7.500 -0.4380 0.01826 0.01046 -0.0705 0.7805 0.0552
-7.250 -0.4161 0.01781 0.01000 -0.0696 0.7737 0.0603
-7.000 -0.3927 0.01746 0.00951 -0.0688 0.7667 0.0661
-6.750 -0.3697 0.01710 0.00911 -0.0680 0.7604 0.0718
-6.500 -0.3457 0.01681 0.00871 -0.0673 0.7530 0.0781
-6.250 -0.3220 0.01650 0.00835 -0.0666 0.7473 0.0844
-6.000 -0.2975 0.01626 0.00800 -0.0660 0.7400 0.0910
-5.750 -0.2735 0.01597 0.00765 -0.0653 0.7338 0.0971
-5.500 -0.2488 0.01576 0.00736 -0.0647 0.7271 0.1039
-5.250 -0.2244 0.01550 0.00704 -0.0641 0.7205 0.1102
-5.000 -0.1996 0.01529 0.00676 -0.0635 0.7145 0.1171
-4.750 -0.1750 0.01507 0.00646 -0.0630 0.7075 0.1235
-4.500 -0.1503 0.01484 0.00618 -0.0624 0.7019 0.1306
-4.250 -0.1254 0.01465 0.00594 -0.0618 0.6950 0.1378
-4.000 -0.1009 0.01443 0.00569 -0.0612 0.6889 0.1459
-3.750 -0.0760 0.01424 0.00545 -0.0607 0.6828 0.1535
-3.500 -0.0514 0.01404 0.00524 -0.0601 0.6763 0.1622
-3.250 -0.0265 0.01386 0.00501 -0.0595 0.6710 0.1726
-3.000 -0.0019 0.01368 0.00484 -0.0589 0.6641 0.1849
-2.750 0.0227 0.01350 0.00465 -0.0584 0.6581 0.1996
-2.500 0.0471 0.01332 0.00451 -0.0577 0.6522 0.2192
-2.250 0.0713 0.01313 0.00437 -0.0571 0.6460 0.2453
-1.750 0.1187 0.01271 0.00414 -0.0557 0.6345 0.3170
-1.500 0.1411 0.01245 0.00404 -0.0547 0.6287 0.3721
-1.250 0.1621 0.01215 0.00397 -0.0534 0.6233 0.4449
-1.000 0.1823 0.01186 0.00396 -0.0519 0.6173 0.5234
-0.750 0.2029 0.01159 0.00392 -0.0503 0.6121 0.6009
-0.500 0.2250 0.01134 0.00395 -0.0490 0.6064 0.6830
-0.250 0.2553 0.01114 0.00402 -0.0492 0.6005 0.7692
0.000 0.3079 0.01114 0.00410 -0.0541 0.5952 0.8440
0.250 0.3646 0.01125 0.00424 -0.0600 0.5883 0.8874
0.500 0.4141 0.01139 0.00431 -0.0644 0.5825 0.9139
0.750 0.4539 0.01156 0.00443 -0.0668 0.5766 0.9370
1.000 0.4944 0.01176 0.00457 -0.0693 0.5704 0.9533
1.250 0.5347 0.01194 0.00465 -0.0719 0.5653 0.9673
1.500 0.5789 0.01208 0.00477 -0.0754 0.5587 0.9795
1.750 0.6210 0.01218 0.00481 -0.0785 0.5528 0.9879
2.000 0.6604 0.01225 0.00483 -0.0813 0.5473 0.9933
2.250 0.6991 0.01233 0.00489 -0.0838 0.5414 0.9987
2.500 0.7262 0.01241 0.00491 -0.0840 0.5363 1.0000
2.750 0.7477 0.01251 0.00499 -0.0830 0.5308 1.0000
3.000 0.7694 0.01260 0.00509 -0.0820 0.5253 1.0000
3.250 0.7912 0.01272 0.00516 -0.0811 0.5205 1.0000
3.500 0.8128 0.01285 0.00530 -0.0801 0.5152 1.0000
3.750 0.8345 0.01298 0.00544 -0.0791 0.5100 1.0000
4.000 0.8563 0.01313 0.00556 -0.0781 0.5054 1.0000
4.250 0.8778 0.01329 0.00574 -0.0770 0.4998 1.0000
4.500 0.8992 0.01345 0.00591 -0.0760 0.4944 1.0000
4.750 0.9210 0.01363 0.00606 -0.0750 0.4900 1.0000
5.000 0.9424 0.01381 0.00630 -0.0740 0.4849 1.0000
5.250 0.9636 0.01400 0.00651 -0.0729 0.4798 1.0000
5.500 0.9852 0.01420 0.00670 -0.0718 0.4754 1.0000
5.750 1.0061 0.01441 0.00697 -0.0707 0.4702 1.0000
6.000 1.0269 0.01462 0.00723 -0.0696 0.4651 1.0000
6.250 1.0482 0.01485 0.00746 -0.0685 0.4609 1.0000
6.500 1.0690 0.01509 0.00775 -0.0674 0.4563 1.0000
6.750 1.0892 0.01533 0.00808 -0.0662 0.4512 1.0000
7.000 1.1099 0.01558 0.00835 -0.0650 0.4467 1.0000
7.250 1.1304 0.01585 0.00866 -0.0638 0.4424 1.0000
7.500 1.1496 0.01612 0.00903 -0.0625 0.4371 1.0000
7.750 1.1696 0.01639 0.00936 -0.0612 0.4326 1.0000
8.000 1.1902 0.01669 0.00969 -0.0601 0.4285 1.0000
8.250 1.2077 0.01699 0.01012 -0.0585 0.4227 1.0000
8.500 1.2257 0.01728 0.01044 -0.0569 0.4166 1.0000
8.750 1.2407 0.01759 0.01084 -0.0548 0.4086 1.0000
9.000 1.2507 0.01792 0.01118 -0.0519 0.3959 1.0000
9.250 1.2542 0.01833 0.01158 -0.0478 0.3795 1.0000
9.500 1.2520 0.01884 0.01205 -0.0430 0.3609 1.0000
9.750 1.2498 0.01961 0.01273 -0.0387 0.3400 1.0000
10.000 1.2512 0.02051 0.01360 -0.0354 0.3174 1.0000
10.250 1.2534 0.02157 0.01461 -0.0325 0.2971 1.0000
10.500 1.2536 0.02289 0.01586 -0.0297 0.2709 1.0000
10.750 1.2507 0.02455 0.01742 -0.0270 0.2425 1.0000
11.000 1.2386 0.02703 0.01969 -0.0240 0.2057 1.0000
11.250 1.2299 0.02953 0.02206 -0.0217 0.1779 1.0000
11.500 1.2167 0.03258 0.02496 -0.0194 0.1472 1.0000
11.750 1.2045 0.03576 0.02802 -0.0176 0.1195 1.0000
12.000 1.1933 0.03902 0.03116 -0.0162 0.0953 1.0000
12.250 1.1836 0.04231 0.03437 -0.0151 0.0754 1.0000
12.500 1.1741 0.04574 0.03771 -0.0142 0.0567 1.0000
12.750 1.1639 0.04940 0.04130 -0.0136 0.0412 1.0000
13.000 1.1591 0.05262 0.04452 -0.0131 0.0332 1.0000
13.250 1.1560 0.05575 0.04766 -0.0129 0.0279 1.0000
13.500 1.1542 0.05882 0.05081 -0.0127 0.0247 1.0000
13.750 1.1511 0.06211 0.05414 -0.0126 0.0220 1.0000
14.000 1.1485 0.06541 0.05750 -0.0126 0.0197 1.0000
14.250 1.1491 0.06839 0.06059 -0.0127 0.0191 1.0000
14.500 1.1478 0.07163 0.06392 -0.0129 0.0176 1.0000
14.750 1.1455 0.07506 0.06742 -0.0132 0.0166 1.0000
15.000 1.1414 0.07880 0.07122 -0.0136 0.0158 1.0000
15.250 1.1408 0.08213 0.07470 -0.0140 0.0153 1.0000
15.500 1.1403 0.08545 0.07813 -0.0144 0.0149 1.0000
15.750 1.1397 0.08884 0.08161 -0.0149 0.0143 1.0000
16.000 1.1380 0.09239 0.08526 -0.0155 0.0138 1.0000
16.250 1.1370 0.09589 0.08884 -0.0161 0.0136 1.0000
16.500 1.1357 0.09947 0.09251 -0.0168 0.0131 1.0000
16.750 1.1336 0.10313 0.09623 -0.0176 0.0126 1.0000
17.000 1.1315 0.10679 0.09995 -0.0184 0.0123 1.0000
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