PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: PSU-90-125WL (psu-90-125wl-il) Reynolds number: 200,000 Max Cl/Cd: 70.28 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-psu-90-125wl-il-200000-n5.txt Download as CSV file: xf-psu-90-125wl-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.250 -0.4677 0.08972 0.08603 -0.0494 1.0000 0.0180
-11.000 -0.5878 0.05778 0.05383 -0.0705 1.0000 0.0162
-10.750 -0.6232 0.05141 0.04724 -0.0737 1.0000 0.0159
-10.500 -0.6493 0.04797 0.04367 -0.0728 1.0000 0.0159
-10.250 -0.6751 0.04605 0.04168 -0.0688 1.0000 0.0159
-10.000 -0.6952 0.04397 0.03946 -0.0649 0.9991 0.0159
-9.750 -0.6816 0.04031 0.03547 -0.0680 0.9907 0.0162
-9.500 -0.6619 0.03769 0.03259 -0.0704 0.9840 0.0167
-9.250 -0.6442 0.03506 0.02965 -0.0717 0.9756 0.0171
-9.000 -0.6218 0.03257 0.02683 -0.0733 0.9694 0.0177
-8.750 -0.6015 0.03018 0.02408 -0.0738 0.9610 0.0180
-8.500 -0.5759 0.02790 0.02142 -0.0750 0.9555 0.0182
-8.250 -0.5524 0.02610 0.01935 -0.0752 0.9477 0.0185
-8.000 -0.5234 0.02443 0.01742 -0.0763 0.9432 0.0189
-7.750 -0.4982 0.02308 0.01588 -0.0764 0.9355 0.0192
-7.500 -0.4686 0.02183 0.01446 -0.0774 0.9304 0.0196
-7.250 -0.4412 0.02078 0.01324 -0.0777 0.9239 0.0200
-7.000 -0.4146 0.01956 0.01194 -0.0781 0.9177 0.0206
-6.750 -0.3867 0.01859 0.01093 -0.0787 0.9122 0.0216
-6.500 -0.3608 0.01792 0.01019 -0.0788 0.9049 0.0228
-6.250 -0.3321 0.01721 0.00938 -0.0793 0.8997 0.0241
-6.000 -0.3075 0.01658 0.00865 -0.0790 0.8924 0.0250
-5.750 -0.2802 0.01600 0.00795 -0.0791 0.8866 0.0260
-5.500 -0.2548 0.01541 0.00728 -0.0789 0.8802 0.0277
-5.250 -0.2290 0.01494 0.00674 -0.0787 0.8738 0.0304
-5.000 -0.2016 0.01448 0.00620 -0.0787 0.8688 0.0355
-4.750 -0.1776 0.01397 0.00576 -0.0781 0.8617 0.0524
-4.500 -0.1524 0.01339 0.00535 -0.0780 0.8562 0.0941
-4.250 -0.1277 0.01292 0.00504 -0.0777 0.8501 0.1380
-4.000 -0.1030 0.01246 0.00477 -0.0774 0.8441 0.1907
-3.750 -0.0768 0.01204 0.00451 -0.0774 0.8393 0.2462
-3.500 -0.0535 0.01160 0.00435 -0.0768 0.8327 0.3175
-3.250 -0.0292 0.01115 0.00420 -0.0764 0.8273 0.4012
-3.000 -0.0045 0.01083 0.00410 -0.0758 0.8219 0.4695
-2.750 0.0205 0.01066 0.00407 -0.0752 0.8158 0.5222
-2.500 0.0473 0.01055 0.00402 -0.0749 0.8108 0.5633
-2.250 0.0733 0.01051 0.00399 -0.0744 0.8047 0.5960
-2.000 0.0999 0.01047 0.00397 -0.0739 0.7988 0.6232
-1.750 0.1272 0.01045 0.00392 -0.0737 0.7937 0.6459
-1.500 0.1532 0.01044 0.00392 -0.0732 0.7871 0.6658
-1.250 0.1805 0.01043 0.00387 -0.0728 0.7816 0.6840
-1.000 0.2070 0.01043 0.00387 -0.0724 0.7754 0.7003
-0.750 0.2337 0.01042 0.00385 -0.0720 0.7690 0.7149
-0.500 0.2608 0.01042 0.00383 -0.0717 0.7631 0.7286
-0.250 0.2869 0.01042 0.00384 -0.0712 0.7558 0.7418
0.000 0.3141 0.01041 0.00381 -0.0709 0.7497 0.7549
0.250 0.3398 0.01041 0.00384 -0.0703 0.7416 0.7678
0.500 0.3669 0.01041 0.00381 -0.0699 0.7351 0.7805
1.000 0.4187 0.01041 0.00384 -0.0688 0.7192 0.8054
1.250 0.4440 0.01041 0.00388 -0.0682 0.7101 0.8179
1.500 0.4696 0.01041 0.00391 -0.0675 0.7013 0.8307
1.750 0.4953 0.01041 0.00391 -0.0669 0.6920 0.8438
2.000 0.5201 0.01041 0.00395 -0.0660 0.6810 0.8578
2.250 0.5451 0.01041 0.00399 -0.0653 0.6699 0.8725
2.500 0.5707 0.01042 0.00401 -0.0646 0.6580 0.8881
2.750 0.5971 0.01043 0.00404 -0.0641 0.6448 0.9047
3.000 0.6250 0.01046 0.00407 -0.0640 0.6297 0.9224
3.250 0.6555 0.01050 0.00412 -0.0645 0.6123 0.9409
3.500 0.6892 0.01059 0.00416 -0.0657 0.5922 0.9594
3.750 0.7239 0.01071 0.00422 -0.0673 0.5699 0.9802
4.000 0.7554 0.01089 0.00432 -0.0683 0.5468 1.0000
4.250 0.7766 0.01112 0.00445 -0.0671 0.5252 1.0000
4.500 0.7980 0.01138 0.00461 -0.0660 0.5029 1.0000
4.750 0.8195 0.01166 0.00481 -0.0649 0.4800 1.0000
5.000 0.8407 0.01198 0.00505 -0.0638 0.4574 1.0000
5.250 0.8620 0.01231 0.00530 -0.0627 0.4343 1.0000
5.500 0.8827 0.01268 0.00557 -0.0615 0.4121 1.0000
5.750 0.9036 0.01304 0.00587 -0.0604 0.3894 1.0000
6.000 0.9237 0.01345 0.00622 -0.0591 0.3676 1.0000
6.250 0.9438 0.01385 0.00656 -0.0579 0.3450 1.0000
6.500 0.9631 0.01430 0.00694 -0.0566 0.3238 1.0000
6.750 0.9826 0.01474 0.00733 -0.0553 0.3025 1.0000
7.000 1.0010 0.01524 0.00778 -0.0539 0.2816 1.0000
7.250 1.0192 0.01574 0.00823 -0.0525 0.2606 1.0000
7.500 1.0367 0.01627 0.00870 -0.0509 0.2404 1.0000
7.750 1.0533 0.01683 0.00921 -0.0493 0.2215 1.0000
8.000 1.0694 0.01739 0.00974 -0.0476 0.2025 1.0000
8.250 1.0839 0.01798 0.01030 -0.0456 0.1853 1.0000
8.500 1.0978 0.01861 0.01090 -0.0436 0.1690 1.0000
8.750 1.1110 0.01931 0.01154 -0.0416 0.1529 1.0000
9.000 1.1238 0.02005 0.01224 -0.0396 0.1352 1.0000
9.250 1.1357 0.02088 0.01299 -0.0376 0.1165 1.0000
9.500 1.1474 0.02175 0.01380 -0.0356 0.1012 1.0000
9.750 1.1588 0.02265 0.01466 -0.0338 0.0874 1.0000
10.000 1.1697 0.02362 0.01561 -0.0319 0.0745 1.0000
10.250 1.1802 0.02464 0.01660 -0.0302 0.0629 1.0000
10.500 1.1910 0.02566 0.01764 -0.0285 0.0540 1.0000
10.750 1.1999 0.02685 0.01882 -0.0268 0.0439 1.0000
11.000 1.2077 0.02816 0.02012 -0.0250 0.0347 1.0000
11.250 1.2149 0.02956 0.02154 -0.0234 0.0279 1.0000
11.500 1.2205 0.03113 0.02314 -0.0217 0.0220 1.0000
11.750 1.2253 0.03282 0.02489 -0.0201 0.0188 1.0000
12.000 1.2302 0.03456 0.02673 -0.0187 0.0163 1.0000
12.250 1.2343 0.03640 0.02867 -0.0174 0.0151 1.0000
12.500 1.2361 0.03852 0.03086 -0.0162 0.0141 1.0000
12.750 1.2393 0.04057 0.03306 -0.0152 0.0134 1.0000
13.000 1.2413 0.04280 0.03543 -0.0143 0.0128 1.0000
13.250 1.2416 0.04529 0.03805 -0.0136 0.0122 1.0000
13.500 1.2418 0.04788 0.04076 -0.0131 0.0116 1.0000
13.750 1.2398 0.05079 0.04379 -0.0129 0.0111 1.0000
14.000 1.2360 0.05405 0.04717 -0.0129 0.0108 1.0000
14.250 1.2310 0.05762 0.05087 -0.0131 0.0105 1.0000
14.500 1.2278 0.06114 0.05455 -0.0136 0.0102 1.0000
14.750 1.2244 0.06486 0.05842 -0.0144 0.0099 1.0000
15.000 1.2190 0.06901 0.06275 -0.0154 0.0098 1.0000
15.250 1.2130 0.07341 0.06730 -0.0168 0.0097 1.0000
15.500 1.2068 0.07802 0.07206 -0.0184 0.0095 1.0000
15.750 1.2001 0.08285 0.07704 -0.0202 0.0094 1.0000
16.000 1.1926 0.08798 0.08232 -0.0223 0.0093 1.0000
16.250 1.1852 0.09320 0.08768 -0.0245 0.0092 1.0000
16.500 1.1779 0.09855 0.09317 -0.0269 0.0091 1.0000
16.750 1.1701 0.10409 0.09885 -0.0295 0.0090 1.0000
17.000 1.1625 0.10970 0.10460 -0.0322 0.0090 1.0000
|
Polar data table (+)
Polar graphs
<< Back to PSU-90-125WL (psu-90-125wl-il)