WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: WASP (smoothed) (waspsm-il) Reynolds number: 200,000 Max Cl/Cd: 69.09 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-waspsm-il-200000-n5.txt Download as CSV file: xf-waspsm-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.750 -0.4433 0.08619 0.08256 -0.0264 1.0000 0.0171
-8.500 -0.4479 0.08180 0.07823 -0.0281 1.0000 0.0171
-8.250 -0.4560 0.07748 0.07398 -0.0297 1.0000 0.0170
-8.000 -0.4650 0.07256 0.06914 -0.0323 1.0000 0.0170
-7.750 -0.4713 0.06597 0.06258 -0.0376 1.0000 0.0171
-7.500 -0.4783 0.05714 0.05370 -0.0443 1.0000 0.0172
-7.250 -0.4971 0.04302 0.03917 -0.0502 1.0000 0.0173
-7.000 -0.5084 0.03347 0.02876 -0.0503 1.0000 0.0178
-6.750 -0.5025 0.02898 0.02357 -0.0488 1.0000 0.0182
-6.500 -0.4766 0.02604 0.02026 -0.0502 0.9970 0.0187
-6.250 -0.4456 0.02419 0.01813 -0.0518 0.9926 0.0194
-6.000 -0.4141 0.02244 0.01607 -0.0533 0.9874 0.0203
-5.750 -0.3833 0.02076 0.01404 -0.0542 0.9814 0.0215
-5.500 -0.3499 0.01945 0.01238 -0.0555 0.9764 0.0233
-5.250 -0.3179 0.01829 0.01109 -0.0567 0.9707 0.0251
-5.000 -0.2825 0.01738 0.01008 -0.0584 0.9666 0.0268
-4.750 -0.2500 0.01647 0.00900 -0.0594 0.9604 0.0287
-4.500 -0.2143 0.01564 0.00803 -0.0610 0.9555 0.0315
-4.250 -0.1783 0.01494 0.00731 -0.0628 0.9503 0.0346
-4.000 -0.1443 0.01431 0.00658 -0.0640 0.9430 0.0377
-3.750 -0.1097 0.01369 0.00592 -0.0654 0.9360 0.0423
-3.500 -0.0764 0.01323 0.00541 -0.0664 0.9269 0.0476
-3.250 -0.0451 0.01275 0.00490 -0.0670 0.9163 0.0539
-3.000 -0.0126 0.01238 0.00449 -0.0679 0.9057 0.0640
-2.750 0.0198 0.01200 0.00412 -0.0687 0.8941 0.0782
-2.500 0.0502 0.01165 0.00383 -0.0691 0.8808 0.0996
-2.250 0.0797 0.01133 0.00356 -0.0693 0.8663 0.1299
-2.000 0.1088 0.01101 0.00334 -0.0695 0.8509 0.1717
-1.750 0.1369 0.01069 0.00316 -0.0694 0.8345 0.2263
-1.500 0.1638 0.01038 0.00301 -0.0691 0.8171 0.2938
-1.250 0.1895 0.01006 0.00291 -0.0686 0.7990 0.3792
-1.000 0.2139 0.00974 0.00284 -0.0676 0.7807 0.4782
-0.750 0.2371 0.00943 0.00278 -0.0664 0.7622 0.5779
-0.500 0.2597 0.00907 0.00273 -0.0648 0.7434 0.6955
-0.250 0.3578 0.00858 0.00262 -0.0797 0.7198 1.0000
0.000 0.3830 0.00870 0.00256 -0.0790 0.6991 1.0000
0.250 0.4080 0.00883 0.00252 -0.0782 0.6780 1.0000
0.500 0.4327 0.00897 0.00249 -0.0773 0.6570 1.0000
0.750 0.4574 0.00912 0.00249 -0.0765 0.6360 1.0000
1.000 0.4820 0.00928 0.00250 -0.0756 0.6152 1.0000
1.250 0.5064 0.00945 0.00252 -0.0747 0.5949 1.0000
1.500 0.5309 0.00962 0.00258 -0.0739 0.5748 1.0000
1.750 0.5553 0.00981 0.00263 -0.0730 0.5556 1.0000
2.000 0.5797 0.01001 0.00271 -0.0722 0.5373 1.0000
2.250 0.6042 0.01021 0.00280 -0.0714 0.5191 1.0000
2.500 0.6286 0.01041 0.00292 -0.0706 0.5013 1.0000
2.750 0.6531 0.01062 0.00304 -0.0698 0.4841 1.0000
3.000 0.6775 0.01083 0.00317 -0.0690 0.4675 1.0000
3.250 0.7019 0.01106 0.00332 -0.0682 0.4516 1.0000
3.500 0.7264 0.01128 0.00349 -0.0675 0.4360 1.0000
3.750 0.7508 0.01152 0.00367 -0.0667 0.4212 1.0000
4.000 0.7752 0.01175 0.00386 -0.0660 0.4067 1.0000
4.250 0.7996 0.01200 0.00408 -0.0652 0.3922 1.0000
4.500 0.8239 0.01225 0.00430 -0.0645 0.3781 1.0000
4.750 0.8482 0.01251 0.00454 -0.0638 0.3645 1.0000
5.000 0.8723 0.01278 0.00479 -0.0630 0.3504 1.0000
5.250 0.8963 0.01307 0.00507 -0.0623 0.3365 1.0000
5.500 0.9202 0.01336 0.00536 -0.0615 0.3234 1.0000
5.750 0.9439 0.01367 0.00566 -0.0607 0.3097 1.0000
6.000 0.9673 0.01400 0.00599 -0.0599 0.2960 1.0000
6.250 0.9907 0.01435 0.00635 -0.0591 0.2834 1.0000
6.500 1.0139 0.01471 0.00671 -0.0582 0.2704 1.0000
6.750 1.0370 0.01507 0.00710 -0.0574 0.2574 1.0000
7.000 1.0596 0.01547 0.00751 -0.0565 0.2436 1.0000
7.250 1.0811 0.01594 0.00794 -0.0555 0.2240 1.0000
7.500 1.1021 0.01645 0.00839 -0.0544 0.2014 1.0000
7.750 1.1229 0.01699 0.00887 -0.0533 0.1834 1.0000
8.000 1.1440 0.01750 0.00939 -0.0523 0.1671 1.0000
8.250 1.1646 0.01807 0.00994 -0.0512 0.1496 1.0000
8.500 1.1841 0.01871 0.01056 -0.0500 0.1306 1.0000
8.750 1.2026 0.01946 0.01124 -0.0487 0.1071 1.0000
9.000 1.2181 0.02046 0.01208 -0.0471 0.0777 1.0000
9.250 1.2311 0.02168 0.01314 -0.0451 0.0527 1.0000
9.500 1.2449 0.02279 0.01422 -0.0432 0.0408 1.0000
9.750 1.2579 0.02391 0.01538 -0.0412 0.0343 1.0000
10.000 1.2716 0.02490 0.01648 -0.0392 0.0301 1.0000
10.500 1.2917 0.02715 0.01892 -0.0345 0.0247 1.0000
10.750 1.2995 0.02827 0.02015 -0.0319 0.0229 1.0000
11.000 1.3046 0.02958 0.02157 -0.0292 0.0217 1.0000
11.250 1.3055 0.03124 0.02333 -0.0264 0.0206 1.0000
11.500 1.3067 0.03299 0.02520 -0.0240 0.0199 1.0000
11.750 1.3096 0.03473 0.02712 -0.0220 0.0192 1.0000
12.000 1.3114 0.03669 0.02922 -0.0204 0.0185 1.0000
12.250 1.3125 0.03884 0.03150 -0.0191 0.0177 1.0000
12.500 1.3130 0.04120 0.03398 -0.0182 0.0170 1.0000
12.750 1.3123 0.04383 0.03674 -0.0177 0.0164 1.0000
13.000 1.3096 0.04685 0.03986 -0.0175 0.0159 1.0000
13.250 1.3041 0.05034 0.04346 -0.0176 0.0155 1.0000
13.500 1.2965 0.05422 0.04744 -0.0178 0.0151 1.0000
13.750 1.2935 0.05769 0.05106 -0.0182 0.0149 1.0000
14.000 1.2898 0.06136 0.05489 -0.0188 0.0146 1.0000
14.250 1.2851 0.06521 0.05889 -0.0195 0.0144 1.0000
14.500 1.2799 0.06922 0.06304 -0.0204 0.0141 1.0000
14.750 1.2741 0.07339 0.06737 -0.0214 0.0139 1.0000
15.000 1.2677 0.07776 0.07188 -0.0226 0.0137 1.0000
15.250 1.2609 0.08230 0.07660 -0.0240 0.0134 1.0000
15.500 1.2537 0.08704 0.08148 -0.0257 0.0132 1.0000
15.750 1.2460 0.09197 0.08655 -0.0275 0.0129 1.0000
16.000 1.2379 0.09710 0.09181 -0.0296 0.0127 1.0000
16.250 1.2296 0.10240 0.09725 -0.0318 0.0125 1.0000
16.500 1.2210 0.10783 0.10280 -0.0343 0.0123 1.0000
16.750 1.2123 0.11341 0.10850 -0.0369 0.0122 1.0000
17.000 1.2036 0.11911 0.11432 -0.0396 0.0120 1.0000
17.250 1.1949 0.12495 0.12027 -0.0425 0.0118 1.0000
17.500 1.1863 0.13087 0.12630 -0.0456 0.0117 1.0000
17.750 1.1773 0.13697 0.13251 -0.0488 0.0115 1.0000
18.000 1.1681 0.14328 0.13892 -0.0523 0.0114 1.0000
18.250 1.1581 0.14996 0.14572 -0.0560 0.0113 1.0000
18.500 1.1468 0.15726 0.15315 -0.0603 0.0112 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WASP (smoothed) (waspsm-il)