PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: PSU-90-125WL (psu-90-125wl-il) Reynolds number: 50,000 Max Cl/Cd: 34.91 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-psu-90-125wl-il-50000-n5.txt Download as CSV file: xf-psu-90-125wl-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: PSU-90-125WL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.750 -0.4222 0.10355 0.09621 -0.0472 1.0000 0.0529
-10.500 -0.4258 0.09899 0.09173 -0.0487 1.0000 0.0525
-10.250 -0.4310 0.09424 0.08705 -0.0505 1.0000 0.0520
-10.000 -0.4390 0.08905 0.08195 -0.0525 1.0000 0.0514
-9.750 -0.4516 0.08293 0.07595 -0.0555 1.0000 0.0507
-9.500 -0.4717 0.07657 0.06966 -0.0589 1.0000 0.0499
-9.250 -0.4972 0.07152 0.06468 -0.0608 1.0000 0.0492
-9.000 -0.5279 0.06794 0.06115 -0.0599 1.0000 0.0488
-8.750 -0.5541 0.06473 0.05793 -0.0578 1.0000 0.0483
-8.500 -0.5769 0.06166 0.05479 -0.0553 1.0000 0.0481
-8.250 -0.5955 0.05868 0.05166 -0.0525 1.0000 0.0478
-8.000 -0.6093 0.05573 0.04850 -0.0497 1.0000 0.0477
-7.750 -0.6179 0.05277 0.04528 -0.0471 1.0000 0.0477
-7.500 -0.6214 0.04988 0.04207 -0.0448 1.0000 0.0477
-7.250 -0.6204 0.04707 0.03892 -0.0428 1.0000 0.0480
-7.000 -0.6151 0.04442 0.03591 -0.0409 1.0000 0.0485
-6.750 -0.6063 0.04196 0.03308 -0.0392 1.0000 0.0491
-6.500 -0.5945 0.03973 0.03045 -0.0376 1.0000 0.0499
-6.250 -0.5683 0.03735 0.02762 -0.0384 0.9959 0.0515
-6.000 -0.5389 0.03542 0.02516 -0.0393 0.9911 0.0546
-5.750 -0.5109 0.03381 0.02354 -0.0403 0.9863 0.0584
-5.500 -0.4813 0.03244 0.02196 -0.0411 0.9819 0.0625
-5.250 -0.4530 0.03114 0.02035 -0.0412 0.9767 0.0667
-5.000 -0.4239 0.02990 0.01912 -0.0421 0.9720 0.0730
-4.750 -0.3974 0.02883 0.01798 -0.0424 0.9665 0.0856
-4.500 -0.3699 0.02761 0.01685 -0.0431 0.9610 0.1109
-4.250 -0.3404 0.02627 0.01592 -0.0448 0.9564 0.1770
-4.000 -0.3176 0.02509 0.01532 -0.0452 0.9499 0.2777
-3.750 -0.2901 0.02431 0.01501 -0.0459 0.9446 0.3841
-3.500 -0.2675 0.02394 0.01502 -0.0449 0.9383 0.4785
-3.250 -0.2428 0.02392 0.01520 -0.0438 0.9320 0.5585
-3.000 -0.2169 0.02405 0.01530 -0.0428 0.9262 0.6211
-2.750 -0.1943 0.02418 0.01536 -0.0413 0.9191 0.6695
-2.500 -0.1647 0.02436 0.01544 -0.0408 0.9140 0.7133
-2.250 -0.1464 0.02447 0.01547 -0.0386 0.9060 0.7484
-2.000 -0.1178 0.02460 0.01548 -0.0379 0.9005 0.7824
-1.750 -0.0968 0.02469 0.01549 -0.0361 0.8929 0.8129
-1.500 -0.0663 0.02478 0.01546 -0.0360 0.8869 0.8431
-1.250 -0.0354 0.02488 0.01544 -0.0362 0.8805 0.8721
-1.000 0.0027 0.02500 0.01542 -0.0379 0.8741 0.9001
-0.750 0.0567 0.02511 0.01536 -0.0428 0.8702 0.9250
-0.500 0.1056 0.02525 0.01535 -0.0473 0.8634 0.9475
-0.250 0.1644 0.02531 0.01525 -0.0536 0.8584 0.9669
0.000 0.2285 0.02525 0.01506 -0.0609 0.8547 0.9825
0.250 0.2675 0.02532 0.01504 -0.0642 0.8455 1.0000
0.500 0.2881 0.02528 0.01492 -0.0637 0.8365 1.0000
0.750 0.3072 0.02529 0.01485 -0.0627 0.8267 1.0000
1.000 0.3198 0.02542 0.01491 -0.0607 0.8153 1.0000
1.250 0.3456 0.02547 0.01488 -0.0606 0.8065 1.0000
1.500 0.3715 0.02554 0.01489 -0.0605 0.7971 1.0000
1.750 0.3913 0.02575 0.01504 -0.0594 0.7858 1.0000
2.000 0.4206 0.02581 0.01506 -0.0597 0.7767 1.0000
2.250 0.4494 0.02585 0.01508 -0.0598 0.7671 1.0000
2.500 0.4711 0.02606 0.01528 -0.0589 0.7551 1.0000
2.750 0.4969 0.02618 0.01541 -0.0585 0.7442 1.0000
3.000 0.5327 0.02601 0.01526 -0.0594 0.7360 1.0000
3.250 0.5544 0.02621 0.01548 -0.0583 0.7230 1.0000
3.500 0.5777 0.02636 0.01566 -0.0574 0.7103 1.0000
3.750 0.6025 0.02645 0.01581 -0.0567 0.6976 1.0000
4.000 0.6288 0.02647 0.01588 -0.0561 0.6849 1.0000
4.250 0.6558 0.02643 0.01590 -0.0555 0.6720 1.0000
4.500 0.6827 0.02638 0.01595 -0.0549 0.6587 1.0000
4.750 0.7081 0.02637 0.01601 -0.0540 0.6442 1.0000
5.000 0.7323 0.02638 0.01610 -0.0530 0.6286 1.0000
5.250 0.7566 0.02638 0.01618 -0.0520 0.6125 1.0000
5.500 0.7818 0.02634 0.01626 -0.0510 0.5956 1.0000
5.750 0.8086 0.02625 0.01623 -0.0502 0.5783 1.0000
6.000 0.8372 0.02608 0.01612 -0.0495 0.5604 1.0000
6.250 0.8592 0.02626 0.01636 -0.0482 0.5398 1.0000
6.500 0.8841 0.02634 0.01651 -0.0472 0.5188 1.0000
6.750 0.9071 0.02656 0.01675 -0.0460 0.4968 1.0000
7.000 0.9292 0.02686 0.01707 -0.0447 0.4741 1.0000
7.250 0.9488 0.02731 0.01754 -0.0432 0.4508 1.0000
7.500 0.9691 0.02776 0.01800 -0.0417 0.4277 1.0000
7.750 0.9848 0.02842 0.01871 -0.0399 0.4041 1.0000
8.000 1.0017 0.02907 0.01933 -0.0381 0.3813 1.0000
8.250 1.0154 0.02987 0.02017 -0.0362 0.3585 1.0000
8.500 1.0289 0.03068 0.02095 -0.0342 0.3371 1.0000
8.750 1.0395 0.03161 0.02192 -0.0319 0.3159 1.0000
9.000 1.0507 0.03258 0.02289 -0.0298 0.2959 1.0000
9.250 1.0598 0.03369 0.02405 -0.0276 0.2760 1.0000
9.500 1.0688 0.03488 0.02527 -0.0255 0.2572 1.0000
9.750 1.0769 0.03614 0.02653 -0.0235 0.2393 1.0000
10.000 1.0850 0.03749 0.02787 -0.0217 0.2228 1.0000
10.250 1.0916 0.03899 0.02943 -0.0198 0.2064 1.0000
10.500 1.0979 0.04059 0.03109 -0.0181 0.1912 1.0000
10.750 1.1035 0.04230 0.03289 -0.0166 0.1770 1.0000
11.000 1.1078 0.04414 0.03477 -0.0150 0.1636 1.0000
11.250 1.1123 0.04606 0.03672 -0.0137 0.1515 1.0000
11.500 1.1149 0.04820 0.03896 -0.0124 0.1396 1.0000
11.750 1.1172 0.05052 0.04142 -0.0113 0.1284 1.0000
12.000 1.1180 0.05303 0.04405 -0.0103 0.1181 1.0000
12.250 1.1173 0.05565 0.04669 -0.0095 0.1090 1.0000
12.500 1.1150 0.05850 0.04963 -0.0090 0.1003 1.0000
12.750 1.1107 0.06181 0.05311 -0.0087 0.0920 1.0000
13.000 1.1061 0.06499 0.05624 -0.0087 0.0851 1.0000
13.250 1.0981 0.06900 0.06052 -0.0091 0.0778 1.0000
13.500 1.0922 0.07272 0.06423 -0.0097 0.0722 1.0000
13.750 1.0842 0.07723 0.06905 -0.0107 0.0668 1.0000
14.000 1.0789 0.08113 0.07293 -0.0117 0.0625 1.0000
14.250 1.0701 0.08626 0.07832 -0.0132 0.0587 1.0000
14.500 1.0605 0.09165 0.08395 -0.0151 0.0555 1.0000
14.750 1.0542 0.09643 0.08881 -0.0170 0.0528 1.0000
15.000 1.0501 0.10092 0.09329 -0.0186 0.0504 1.0000
15.250 1.0348 0.10823 0.10093 -0.0220 0.0493 1.0000
15.500 1.0174 0.11636 0.10932 -0.0263 0.0486 1.0000
15.750 0.9965 0.12580 0.11899 -0.0316 0.0485 1.0000
16.000 0.9709 0.13719 0.13050 -0.0382 0.0489 1.0000
16.250 0.9450 0.14975 0.14311 -0.0454 0.0494 1.0000
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