PSU-90-125WL (psu-90-125wl-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: PSU-90-125WL (psu-90-125wl-il) Reynolds number: 200,000 Max Cl/Cd: 75.81 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-psu-90-125wl-il-200000.txt Download as CSV file: xf-psu-90-125wl-il-200000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.4169 0.09961 0.09605 -0.0486 1.0000 0.0665
-10.250 -0.4442 0.09218 0.08873 -0.0564 1.0000 0.0671
-10.000 -0.4524 0.08619 0.08281 -0.0570 1.0000 0.0680
-9.750 -0.4361 0.08563 0.08225 -0.0525 1.0000 0.0691
-9.500 -0.4246 0.08472 0.08135 -0.0498 1.0000 0.0710
-9.250 -0.4283 0.08163 0.07830 -0.0499 1.0000 0.0727
-9.000 -0.4412 0.07767 0.07442 -0.0509 1.0000 0.0740
-8.750 -0.4711 0.07275 0.06965 -0.0522 1.0000 0.0735
-8.500 -0.5305 0.07065 0.06767 -0.0480 1.0000 0.0721
-8.250 -0.5465 0.06623 0.06318 -0.0511 0.9955 0.0730
-8.000 -0.5637 0.05670 0.05276 -0.0640 0.9800 0.0810
-7.750 -0.5636 0.03888 0.03384 -0.0656 0.9732 0.0420
-7.500 -0.5453 0.03442 0.02890 -0.0664 0.9670 0.0402
-7.250 -0.5239 0.02924 0.02277 -0.0666 0.9612 0.0368
-7.000 -0.4905 0.02678 0.01987 -0.0682 0.9584 0.0362
-6.750 -0.4649 0.02493 0.01778 -0.0682 0.9530 0.0364
-6.500 -0.4346 0.02325 0.01594 -0.0691 0.9486 0.0370
-6.250 -0.3998 0.02187 0.01447 -0.0707 0.9458 0.0383
-6.000 -0.3623 0.02082 0.01334 -0.0729 0.9438 0.0408
-5.750 -0.3382 0.01997 0.01241 -0.0723 0.9372 0.0424
-5.500 -0.3049 0.01902 0.01136 -0.0735 0.9335 0.0441
-5.250 -0.2708 0.01763 0.01001 -0.0752 0.9309 0.0476
-5.000 -0.2334 0.01679 0.00912 -0.0772 0.9288 0.0544
-4.750 -0.2144 0.01604 0.00842 -0.0759 0.9209 0.0695
-4.500 -0.1862 0.01451 0.00755 -0.0768 0.9170 0.1847
-4.250 -0.1521 0.01376 0.00712 -0.0785 0.9144 0.2718
-4.000 -0.1320 0.01334 0.00700 -0.0774 0.9071 0.3482
-3.750 -0.1039 0.01277 0.00681 -0.0777 0.9027 0.4447
-3.500 -0.0722 0.01237 0.00673 -0.0783 0.8996 0.5351
-3.250 -0.0503 0.01237 0.00683 -0.0770 0.8926 0.5884
-3.000 -0.0213 0.01231 0.00681 -0.0768 0.8878 0.6297
-2.750 0.0113 0.01223 0.00672 -0.0772 0.8844 0.6635
-2.500 0.0338 0.01232 0.00682 -0.0759 0.8773 0.6876
-2.250 0.0625 0.01230 0.00676 -0.0756 0.8722 0.7106
-2.000 0.0942 0.01223 0.00666 -0.0758 0.8686 0.7315
-1.750 0.1152 0.01234 0.00678 -0.0742 0.8606 0.7490
-1.500 0.1441 0.01228 0.00670 -0.0739 0.8557 0.7664
-1.250 0.1699 0.01230 0.00670 -0.0731 0.8499 0.7825
-1.000 0.1945 0.01230 0.00670 -0.0720 0.8430 0.7979
-0.750 0.2239 0.01222 0.00658 -0.0718 0.8385 0.8125
-0.500 0.2453 0.01227 0.00665 -0.0702 0.8303 0.8267
-0.250 0.2730 0.01218 0.00653 -0.0696 0.8246 0.8406
0.000 0.2959 0.01219 0.00655 -0.0683 0.8170 0.8547
0.250 0.3217 0.01211 0.00645 -0.0674 0.8104 0.8687
0.500 0.3453 0.01209 0.00643 -0.0661 0.8030 0.8830
0.750 0.3702 0.01201 0.00635 -0.0650 0.7956 0.8971
1.000 0.3954 0.01196 0.00630 -0.0640 0.7882 0.9113
1.250 0.4233 0.01187 0.00621 -0.0635 0.7803 0.9255
1.500 0.4549 0.01182 0.00616 -0.0640 0.7722 0.9389
1.750 0.4927 0.01172 0.00603 -0.0656 0.7641 0.9504
2.000 0.5314 0.01167 0.00598 -0.0678 0.7542 0.9615
2.250 0.5738 0.01155 0.00582 -0.0705 0.7460 0.9715
2.500 0.6185 0.01147 0.00575 -0.0740 0.7346 0.9795
2.750 0.6628 0.01137 0.00566 -0.0775 0.7227 0.9881
3.000 0.7069 0.01125 0.00554 -0.0809 0.7102 0.9975
3.250 0.7285 0.01117 0.00544 -0.0801 0.6979 1.0000
3.500 0.7427 0.01113 0.00536 -0.0776 0.6851 1.0000
3.750 0.7595 0.01113 0.00533 -0.0756 0.6712 1.0000
4.000 0.7787 0.01115 0.00533 -0.0739 0.6553 1.0000
4.250 0.7997 0.01120 0.00536 -0.0725 0.6377 1.0000
4.500 0.8219 0.01126 0.00539 -0.0714 0.6185 1.0000
4.750 0.8449 0.01136 0.00543 -0.0703 0.5983 1.0000
5.000 0.8669 0.01152 0.00554 -0.0691 0.5755 1.0000
5.250 0.8891 0.01174 0.00565 -0.0680 0.5521 1.0000
5.500 0.9105 0.01201 0.00587 -0.0667 0.5271 1.0000
5.750 0.9315 0.01234 0.00610 -0.0655 0.5020 1.0000
6.000 0.9520 0.01271 0.00637 -0.0641 0.4769 1.0000
6.250 0.9719 0.01309 0.00668 -0.0627 0.4512 1.0000
6.500 0.9912 0.01351 0.00704 -0.0613 0.4254 1.0000
6.750 1.0099 0.01397 0.00741 -0.0597 0.4003 1.0000
7.000 1.0278 0.01446 0.00781 -0.0581 0.3747 1.0000
7.250 1.0454 0.01495 0.00825 -0.0564 0.3494 1.0000
7.500 1.0620 0.01550 0.00873 -0.0546 0.3249 1.0000
7.750 1.0778 0.01608 0.00924 -0.0527 0.3008 1.0000
8.000 1.0933 0.01667 0.00977 -0.0509 0.2773 1.0000
8.250 1.1071 0.01733 0.01035 -0.0487 0.2554 1.0000
8.500 1.1204 0.01796 0.01095 -0.0465 0.2342 1.0000
8.750 1.1315 0.01866 0.01160 -0.0440 0.2142 1.0000
9.000 1.1417 0.01944 0.01231 -0.0415 0.1948 1.0000
9.250 1.1528 0.02021 0.01304 -0.0392 0.1746 1.0000
9.500 1.1617 0.02111 0.01384 -0.0368 0.1551 1.0000
9.750 1.1723 0.02199 0.01468 -0.0347 0.1360 1.0000
10.000 1.1825 0.02294 0.01560 -0.0327 0.1203 1.0000
10.250 1.1919 0.02398 0.01665 -0.0307 0.1066 1.0000
10.500 1.2007 0.02510 0.01776 -0.0288 0.0937 1.0000
10.750 1.2086 0.02634 0.01898 -0.0269 0.0804 1.0000
11.000 1.2145 0.02777 0.02038 -0.0249 0.0667 1.0000
11.250 1.2151 0.02966 0.02218 -0.0228 0.0528 1.0000
11.500 1.2123 0.03196 0.02445 -0.0204 0.0409 1.0000
11.750 1.2109 0.03420 0.02672 -0.0185 0.0349 1.0000
12.000 1.2096 0.03657 0.02917 -0.0167 0.0319 1.0000
12.250 1.2113 0.03874 0.03144 -0.0153 0.0294 1.0000
12.500 1.2098 0.04128 0.03402 -0.0140 0.0275 1.0000
12.750 1.2067 0.04415 0.03694 -0.0127 0.0262 1.0000
13.000 1.2115 0.04632 0.03927 -0.0119 0.0251 1.0000
13.250 1.2153 0.04862 0.04169 -0.0111 0.0241 1.0000
13.500 1.2179 0.05105 0.04422 -0.0106 0.0228 1.0000
13.750 1.2199 0.05363 0.04685 -0.0103 0.0219 1.0000
14.000 1.2218 0.05639 0.04966 -0.0098 0.0211 1.0000
14.250 1.2271 0.05920 0.05255 -0.0089 0.0205 1.0000
14.500 1.2299 0.06204 0.05557 -0.0087 0.0203 1.0000
14.750 1.2311 0.06516 0.05888 -0.0087 0.0200 1.0000
15.000 1.2308 0.06856 0.06249 -0.0088 0.0197 1.0000
15.250 1.2285 0.07231 0.06644 -0.0092 0.0196 1.0000
15.500 1.2223 0.07668 0.07105 -0.0101 0.0193 1.0000
15.750 1.2155 0.08126 0.07585 -0.0113 0.0192 1.0000
16.000 1.2060 0.08641 0.08122 -0.0130 0.0192 1.0000
16.250 1.1934 0.09222 0.08727 -0.0153 0.0191 1.0000
16.500 1.1801 0.09837 0.09363 -0.0182 0.0192 1.0000
16.750 1.1635 0.10538 0.10087 -0.0218 0.0192 1.0000
17.000 1.1457 0.11296 0.10867 -0.0260 0.0193 1.0000
17.250 1.1274 0.12099 0.11690 -0.0308 0.0195 1.0000
17.500 1.1075 0.12977 0.12587 -0.0363 0.0197 1.0000
17.750 1.0845 0.13978 0.13605 -0.0429 0.0199 1.0000
18.000 1.0623 0.15013 0.14655 -0.0496 0.0202 1.0000
18.250 1.0376 0.16175 0.15829 -0.0571 0.0205 1.0000
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