WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WASP (smoothed) (waspsm-il) Reynolds number: 500,000 Max Cl/Cd: 96.01 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-waspsm-il-500000.txt Download as CSV file: xf-waspsm-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.000 -0.3330 0.09647 0.09426 -0.0278 1.0000 0.0237
-9.750 -0.3339 0.09227 0.09007 -0.0289 1.0000 0.0237
-9.500 -0.3432 0.08603 0.08386 -0.0297 1.0000 0.0242
-9.250 -0.3406 0.08283 0.08067 -0.0295 1.0000 0.0245
-9.000 -0.3382 0.07972 0.07758 -0.0295 1.0000 0.0248
-8.750 -0.3373 0.07636 0.07424 -0.0298 1.0000 0.0251
-8.500 -0.3371 0.07302 0.07092 -0.0301 1.0000 0.0255
-8.250 -0.3393 0.06935 0.06727 -0.0306 1.0000 0.0259
-8.000 -0.3435 0.06558 0.06354 -0.0312 1.0000 0.0263
-7.000 -0.5101 0.03619 0.03326 -0.0470 1.0000 0.0180
-6.750 -0.4901 0.02634 0.02249 -0.0519 0.9961 0.0176
-6.500 -0.4610 0.02256 0.01811 -0.0537 0.9927 0.0179
-6.250 -0.4311 0.01947 0.01449 -0.0551 0.9890 0.0184
-6.000 -0.4009 0.01712 0.01187 -0.0563 0.9853 0.0193
-5.750 -0.3668 0.01651 0.01120 -0.0579 0.9812 0.0206
-5.500 -0.3309 0.01562 0.01017 -0.0596 0.9783 0.0220
-5.250 -0.2981 0.01469 0.00906 -0.0605 0.9737 0.0232
-5.000 -0.2653 0.01317 0.00736 -0.0616 0.9701 0.0248
-4.750 -0.2292 0.01245 0.00660 -0.0634 0.9675 0.0267
-4.500 -0.1930 0.01198 0.00609 -0.0650 0.9638 0.0292
-4.250 -0.1573 0.01131 0.00533 -0.0666 0.9589 0.0316
-4.000 -0.1182 0.01060 0.00461 -0.0690 0.9553 0.0351
-3.750 -0.0792 0.01027 0.00423 -0.0713 0.9500 0.0388
-3.500 -0.0447 0.00964 0.00358 -0.0727 0.9418 0.0440
-3.250 -0.0116 0.00939 0.00327 -0.0736 0.9318 0.0498
-3.000 0.0198 0.00900 0.00290 -0.0742 0.9209 0.0603
-2.750 0.0494 0.00871 0.00260 -0.0744 0.9085 0.0745
-2.500 0.0772 0.00841 0.00237 -0.0742 0.8946 0.0984
-2.250 0.1038 0.00814 0.00218 -0.0738 0.8792 0.1354
-2.000 0.1296 0.00787 0.00204 -0.0732 0.8624 0.1861
-1.750 0.1549 0.00761 0.00192 -0.0725 0.8447 0.2474
-1.500 0.1796 0.00735 0.00182 -0.0718 0.8263 0.3225
-1.250 0.2034 0.00709 0.00176 -0.0708 0.8079 0.4127
-1.000 0.2263 0.00685 0.00173 -0.0696 0.7893 0.5081
-0.750 0.2479 0.00660 0.00171 -0.0680 0.7702 0.6036
-0.500 0.2665 0.00625 0.00171 -0.0657 0.7510 0.7301
-0.250 0.3774 0.00586 0.00172 -0.0842 0.7273 1.0000
0.000 0.4021 0.00597 0.00169 -0.0833 0.7051 1.0000
0.250 0.4267 0.00610 0.00166 -0.0825 0.6831 1.0000
0.500 0.4514 0.00622 0.00166 -0.0816 0.6609 1.0000
0.750 0.4760 0.00636 0.00166 -0.0807 0.6393 1.0000
1.000 0.5006 0.00650 0.00168 -0.0799 0.6166 1.0000
1.250 0.5250 0.00666 0.00171 -0.0790 0.5949 1.0000
1.500 0.5496 0.00682 0.00175 -0.0782 0.5733 1.0000
1.750 0.5741 0.00699 0.00180 -0.0774 0.5528 1.0000
2.000 0.5989 0.00715 0.00187 -0.0766 0.5334 1.0000
2.250 0.6237 0.00732 0.00194 -0.0759 0.5146 1.0000
2.500 0.6486 0.00749 0.00203 -0.0751 0.4971 1.0000
2.750 0.6735 0.00766 0.00212 -0.0744 0.4806 1.0000
3.000 0.6984 0.00784 0.00222 -0.0737 0.4643 1.0000
3.250 0.7233 0.00802 0.00235 -0.0730 0.4488 1.0000
3.500 0.7483 0.00820 0.00247 -0.0724 0.4343 1.0000
3.750 0.7732 0.00838 0.00260 -0.0717 0.4194 1.0000
4.000 0.7981 0.00858 0.00274 -0.0710 0.4045 1.0000
4.250 0.8231 0.00877 0.00290 -0.0704 0.3906 1.0000
4.500 0.8480 0.00897 0.00306 -0.0697 0.3765 1.0000
4.750 0.8727 0.00918 0.00323 -0.0691 0.3619 1.0000
5.000 0.8974 0.00939 0.00341 -0.0684 0.3478 1.0000
5.250 0.9220 0.00962 0.00362 -0.0677 0.3342 1.0000
5.500 0.9465 0.00986 0.00382 -0.0670 0.3200 1.0000
5.750 0.9707 0.01011 0.00405 -0.0663 0.3052 1.0000
6.000 0.9949 0.01038 0.00428 -0.0656 0.2909 1.0000
6.250 1.0184 0.01069 0.00454 -0.0648 0.2726 1.0000
6.500 1.0416 0.01103 0.00480 -0.0639 0.2508 1.0000
6.750 1.0648 0.01138 0.00508 -0.0631 0.2319 1.0000
7.000 1.0878 0.01174 0.00539 -0.0623 0.2154 1.0000
7.250 1.1105 0.01213 0.00573 -0.0614 0.1990 1.0000
7.500 1.1332 0.01252 0.00607 -0.0605 0.1834 1.0000
7.750 1.1558 0.01291 0.00643 -0.0596 0.1688 1.0000
8.000 1.1782 0.01332 0.00682 -0.0587 0.1539 1.0000
8.250 1.1999 0.01378 0.00724 -0.0578 0.1364 1.0000
8.500 1.2200 0.01439 0.00774 -0.0565 0.1129 1.0000
8.750 1.2357 0.01540 0.00848 -0.0548 0.0715 1.0000
9.000 1.2487 0.01665 0.00950 -0.0525 0.0410 1.0000
9.250 1.2650 0.01757 0.01041 -0.0507 0.0316 1.0000
9.500 1.2797 0.01861 0.01149 -0.0486 0.0265 1.0000
9.750 1.2978 0.01928 0.01224 -0.0471 0.0241 1.0000
10.000 1.3129 0.02017 0.01318 -0.0452 0.0218 1.0000
10.250 1.3229 0.02140 0.01450 -0.0425 0.0200 1.0000
10.500 1.3379 0.02218 0.01538 -0.0406 0.0191 1.0000
10.750 1.3501 0.02308 0.01637 -0.0384 0.0181 1.0000
11.000 1.3589 0.02401 0.01737 -0.0356 0.0173 1.0000
11.250 1.3657 0.02505 0.01849 -0.0326 0.0165 1.0000
11.500 1.3660 0.02655 0.02007 -0.0292 0.0158 1.0000
11.750 1.3572 0.02886 0.02251 -0.0253 0.0151 1.0000
12.000 1.3669 0.02996 0.02372 -0.0236 0.0147 1.0000
12.250 1.3722 0.03147 0.02534 -0.0218 0.0143 1.0000
12.500 1.3755 0.03327 0.02725 -0.0201 0.0139 1.0000
12.750 1.3778 0.03528 0.02937 -0.0188 0.0135 1.0000
13.000 1.3793 0.03750 0.03170 -0.0177 0.0132 1.0000
13.250 1.3800 0.03993 0.03424 -0.0169 0.0128 1.0000
13.500 1.3799 0.04259 0.03700 -0.0165 0.0125 1.0000
13.750 1.3785 0.04550 0.04003 -0.0163 0.0122 1.0000
14.000 1.3756 0.04873 0.04335 -0.0163 0.0120 1.0000
14.250 1.3706 0.05228 0.04701 -0.0165 0.0118 1.0000
14.500 1.3629 0.05623 0.05106 -0.0167 0.0115 1.0000
14.750 1.3516 0.06060 0.05557 -0.0167 0.0113 1.0000
15.000 1.3417 0.06499 0.06010 -0.0171 0.0111 1.0000
15.250 1.3375 0.06899 0.06425 -0.0184 0.0110 1.0000
15.500 1.3319 0.07327 0.06867 -0.0198 0.0109 1.0000
15.750 1.3252 0.07782 0.07336 -0.0214 0.0107 1.0000
16.000 1.3176 0.08263 0.07832 -0.0232 0.0106 1.0000
16.250 1.3090 0.08769 0.08351 -0.0252 0.0104 1.0000
16.500 1.2994 0.09302 0.08897 -0.0274 0.0103 1.0000
16.750 1.2892 0.09859 0.09468 -0.0297 0.0102 1.0000
17.000 1.2783 0.10441 0.10065 -0.0323 0.0101 1.0000
17.250 1.2663 0.11053 0.10691 -0.0351 0.0100 1.0000
17.500 1.2536 0.11694 0.11345 -0.0382 0.0100 1.0000
17.750 1.2404 0.12367 0.12032 -0.0416 0.0099 1.0000
18.000 1.2262 0.13081 0.12760 -0.0453 0.0099 1.0000
18.250 1.2111 0.13831 0.13525 -0.0494 0.0099 1.0000
18.500 1.1946 0.14645 0.14353 -0.0540 0.0099 1.0000
18.750 1.1767 0.15530 0.15254 -0.0592 0.0099 1.0000
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