WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WASP (smoothed) (waspsm-il) Reynolds number: 1,000,000 Max Cl/Cd: 108.06 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-waspsm-il-1000000-n5.txt Download as CSV file: xf-waspsm-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WASP (smoothed)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.9535 0.03419 0.03172 -0.0644 1.0000 0.0057
-12.000 -0.9503 0.03064 0.02793 -0.0644 1.0000 0.0058
-11.750 -0.9403 0.02820 0.02529 -0.0639 1.0000 0.0059
-11.500 -0.9271 0.02628 0.02317 -0.0631 1.0000 0.0060
-11.250 -0.9115 0.02475 0.02149 -0.0623 1.0000 0.0061
-11.000 -0.8946 0.02343 0.02004 -0.0613 1.0000 0.0062
-10.750 -0.8770 0.02226 0.01873 -0.0603 1.0000 0.0063
-10.500 -0.8591 0.02118 0.01753 -0.0591 1.0000 0.0065
-10.250 -0.8412 0.02017 0.01639 -0.0578 1.0000 0.0066
-10.000 -0.8147 0.01908 0.01515 -0.0584 0.9992 0.0068
-9.750 -0.7859 0.01803 0.01394 -0.0593 0.9977 0.0069
-9.500 -0.7570 0.01710 0.01287 -0.0601 0.9956 0.0071
-9.000 -0.7068 0.01554 0.01108 -0.0597 0.9816 0.0073
-8.750 -0.6780 0.01487 0.01029 -0.0602 0.9767 0.0074
-8.500 -0.6489 0.01396 0.00925 -0.0609 0.9730 0.0077
-8.250 -0.6175 0.01326 0.00845 -0.0619 0.9700 0.0080
-8.000 -0.5840 0.01270 0.00783 -0.0633 0.9674 0.0084
-7.750 -0.5491 0.01221 0.00727 -0.0650 0.9644 0.0087
-7.500 -0.5128 0.01174 0.00673 -0.0670 0.9607 0.0091
-7.250 -0.4736 0.01127 0.00619 -0.0696 0.9574 0.0096
-7.000 -0.4324 0.01084 0.00568 -0.0727 0.9541 0.0100
-6.750 -0.3950 0.01043 0.00520 -0.0749 0.9478 0.0105
-6.500 -0.3584 0.01002 0.00474 -0.0769 0.9403 0.0113
-6.250 -0.3273 0.00977 0.00445 -0.0776 0.9309 0.0121
-6.000 -0.2967 0.00954 0.00415 -0.0782 0.9207 0.0130
-5.750 -0.2675 0.00934 0.00388 -0.0784 0.9087 0.0136
-5.500 -0.2402 0.00906 0.00354 -0.0782 0.8945 0.0146
-5.250 -0.2135 0.00886 0.00328 -0.0778 0.8781 0.0157
-5.000 -0.1874 0.00871 0.00304 -0.0773 0.8593 0.0167
-4.750 -0.1617 0.00859 0.00282 -0.0767 0.8396 0.0177
-4.500 -0.1366 0.00847 0.00260 -0.0759 0.8201 0.0187
-4.250 -0.1116 0.00833 0.00241 -0.0751 0.8008 0.0207
-4.000 -0.0865 0.00824 0.00224 -0.0744 0.7821 0.0226
-3.750 -0.0613 0.00818 0.00208 -0.0736 0.7634 0.0240
-3.500 -0.0365 0.00807 0.00192 -0.0728 0.7452 0.0276
-3.250 -0.0111 0.00801 0.00178 -0.0721 0.7267 0.0304
-3.000 0.0141 0.00793 0.00165 -0.0714 0.7084 0.0348
-2.750 0.0393 0.00789 0.00154 -0.0707 0.6891 0.0393
-2.500 0.0644 0.00783 0.00144 -0.0700 0.6706 0.0469
-2.250 0.0898 0.00778 0.00135 -0.0693 0.6517 0.0547
-2.000 0.1153 0.00774 0.00127 -0.0687 0.6328 0.0644
-1.750 0.1406 0.00770 0.00120 -0.0680 0.6140 0.0777
-1.500 0.1657 0.00765 0.00114 -0.0673 0.5954 0.0975
-1.250 0.1909 0.00759 0.00109 -0.0667 0.5758 0.1232
-1.000 0.2162 0.00755 0.00106 -0.0660 0.5576 0.1489
-0.750 0.2414 0.00750 0.00103 -0.0654 0.5400 0.1814
-0.500 0.2665 0.00745 0.00101 -0.0647 0.5223 0.2171
-0.250 0.2916 0.00740 0.00101 -0.0641 0.5053 0.2580
0.000 0.3167 0.00732 0.00101 -0.0635 0.4904 0.3077
0.250 0.3413 0.00721 0.00103 -0.0628 0.4760 0.3741
0.500 0.3661 0.00713 0.00106 -0.0621 0.4610 0.4350
0.750 0.3910 0.00708 0.00110 -0.0614 0.4464 0.4900
1.000 0.4156 0.00702 0.00114 -0.0606 0.4318 0.5507
1.250 0.4394 0.00691 0.00120 -0.0597 0.4180 0.6271
1.500 0.4616 0.00674 0.00126 -0.0584 0.4051 0.7207
2.000 0.6010 0.00656 0.00151 -0.0778 0.3664 1.0000
2.250 0.6267 0.00669 0.00158 -0.0772 0.3537 1.0000
2.500 0.6525 0.00683 0.00165 -0.0767 0.3419 1.0000
2.750 0.6785 0.00695 0.00172 -0.0762 0.3312 1.0000
3.000 0.7042 0.00709 0.00181 -0.0757 0.3191 1.0000
3.250 0.7298 0.00724 0.00191 -0.0752 0.3069 1.0000
3.500 0.7554 0.00740 0.00201 -0.0747 0.2963 1.0000
3.750 0.7809 0.00756 0.00212 -0.0741 0.2847 1.0000
4.000 0.8063 0.00773 0.00224 -0.0736 0.2723 1.0000
4.250 0.8318 0.00789 0.00238 -0.0730 0.2613 1.0000
4.500 0.8572 0.00807 0.00251 -0.0725 0.2515 1.0000
5.000 0.9075 0.00845 0.00281 -0.0713 0.2291 1.0000
5.250 0.9325 0.00865 0.00299 -0.0708 0.2185 1.0000
5.500 0.9574 0.00886 0.00317 -0.0701 0.2079 1.0000
5.750 0.9811 0.00918 0.00338 -0.0694 0.1881 1.0000
6.000 1.0041 0.00955 0.00364 -0.0685 0.1654 1.0000
6.250 1.0275 0.00990 0.00390 -0.0677 0.1472 1.0000
6.500 1.0507 0.01025 0.00416 -0.0668 0.1312 1.0000
6.750 1.0743 0.01057 0.00443 -0.0660 0.1182 1.0000
7.000 1.0976 0.01091 0.00473 -0.0652 0.1049 1.0000
7.250 1.1198 0.01135 0.00507 -0.0643 0.0873 1.0000
7.500 1.1400 0.01197 0.00554 -0.0630 0.0617 1.0000
7.750 1.1602 0.01259 0.00604 -0.0617 0.0419 1.0000
8.000 1.1817 0.01307 0.00648 -0.0606 0.0318 1.0000
8.250 1.2036 0.01352 0.00691 -0.0596 0.0255 1.0000
8.500 1.2254 0.01397 0.00734 -0.0586 0.0209 1.0000
8.750 1.2476 0.01436 0.00775 -0.0577 0.0182 1.0000
9.000 1.2689 0.01483 0.00821 -0.0567 0.0154 1.0000
9.250 1.2908 0.01523 0.00865 -0.0557 0.0139 1.0000
9.500 1.3119 0.01568 0.00912 -0.0546 0.0124 1.0000
9.750 1.3324 0.01619 0.00964 -0.0535 0.0111 1.0000
10.000 1.3534 0.01662 0.01012 -0.0524 0.0105 1.0000
10.250 1.3738 0.01709 0.01062 -0.0513 0.0098 1.0000
10.500 1.3933 0.01761 0.01117 -0.0500 0.0091 1.0000
10.750 1.4116 0.01820 0.01181 -0.0486 0.0084 1.0000
11.000 1.4298 0.01878 0.01243 -0.0472 0.0080 1.0000
11.250 1.4480 0.01932 0.01303 -0.0458 0.0077 1.0000
11.500 1.4652 0.01990 0.01367 -0.0443 0.0074 1.0000
11.750 1.4814 0.02052 0.01435 -0.0426 0.0071 1.0000
12.000 1.4960 0.02118 0.01506 -0.0407 0.0068 1.0000
12.250 1.5073 0.02186 0.01581 -0.0382 0.0065 1.0000
12.500 1.5172 0.02261 0.01662 -0.0356 0.0063 1.0000
12.750 1.5255 0.02351 0.01757 -0.0330 0.0060 1.0000
13.000 1.5318 0.02458 0.01873 -0.0304 0.0057 1.0000
13.250 1.5414 0.02550 0.01972 -0.0284 0.0056 1.0000
13.500 1.5500 0.02654 0.02084 -0.0264 0.0054 1.0000
13.750 1.5573 0.02774 0.02213 -0.0246 0.0053 1.0000
14.000 1.5635 0.02910 0.02357 -0.0229 0.0052 1.0000
14.250 1.5686 0.03064 0.02521 -0.0214 0.0050 1.0000
14.500 1.5726 0.03239 0.02705 -0.0201 0.0049 1.0000
14.750 1.5756 0.03435 0.02911 -0.0191 0.0048 1.0000
15.000 1.5773 0.03658 0.03143 -0.0184 0.0046 1.0000
15.250 1.5777 0.03909 0.03405 -0.0179 0.0045 1.0000
15.500 1.5765 0.04194 0.03699 -0.0178 0.0044 1.0000
15.750 1.5735 0.04515 0.04031 -0.0180 0.0043 1.0000
16.000 1.5685 0.04877 0.04404 -0.0186 0.0043 1.0000
16.250 1.5611 0.05287 0.04825 -0.0194 0.0042 1.0000
16.500 1.5511 0.05747 0.05298 -0.0207 0.0041 1.0000
16.750 1.5389 0.06255 0.05818 -0.0222 0.0041 1.0000
17.000 1.5241 0.06815 0.06391 -0.0241 0.0040 1.0000
17.250 1.5073 0.07421 0.07011 -0.0263 0.0040 1.0000
17.500 1.4886 0.08070 0.07673 -0.0287 0.0040 1.0000
17.750 1.4687 0.08752 0.08368 -0.0313 0.0039 1.0000
18.000 1.4480 0.09465 0.09093 -0.0342 0.0039 1.0000
18.250 1.4269 0.10189 0.09830 -0.0372 0.0039 1.0000
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