WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: WASP (smoothed) (waspsm-il) Reynolds number: 1,000,000 Max Cl/Cd: 115.78 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-waspsm-il-1000000.txt Download as CSV file: xf-waspsm-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.4615 0.09316 0.09151 -0.0211 1.0000 0.0140
-9.250 -0.6816 0.03375 0.03160 -0.0573 1.0000 0.0094
-9.000 -0.6950 0.02716 0.02442 -0.0556 1.0000 0.0095
-8.750 -0.6900 0.02463 0.02160 -0.0531 1.0000 0.0097
-8.500 -0.6629 0.02236 0.01902 -0.0546 0.9987 0.0100
-8.250 -0.6328 0.02063 0.01701 -0.0562 0.9970 0.0102
-8.000 -0.6078 0.01712 0.01298 -0.0574 0.9948 0.0106
-7.750 -0.5790 0.01577 0.01148 -0.0582 0.9918 0.0111
-7.500 -0.5472 0.01506 0.01068 -0.0593 0.9886 0.0115
-7.250 -0.5172 0.01438 0.00991 -0.0600 0.9845 0.0119
-7.000 -0.4862 0.01366 0.00908 -0.0608 0.9807 0.0123
-6.750 -0.4536 0.01293 0.00825 -0.0619 0.9778 0.0128
-6.500 -0.4236 0.01233 0.00756 -0.0624 0.9733 0.0133
-6.250 -0.3900 0.01189 0.00704 -0.0636 0.9702 0.0137
-6.000 -0.3568 0.01066 0.00567 -0.0650 0.9677 0.0149
-5.750 -0.3200 0.01029 0.00527 -0.0669 0.9648 0.0160
-5.500 -0.2827 0.00999 0.00494 -0.0690 0.9607 0.0173
-5.250 -0.2418 0.00972 0.00462 -0.0719 0.9572 0.0183
-5.000 -0.2015 0.00898 0.00381 -0.0747 0.9530 0.0205
-4.750 -0.1681 0.00875 0.00355 -0.0759 0.9444 0.0222
-4.500 -0.1337 0.00856 0.00331 -0.0772 0.9364 0.0235
-4.250 -0.1046 0.00816 0.00285 -0.0774 0.9256 0.0262
-4.000 -0.0771 0.00800 0.00266 -0.0772 0.9135 0.0286
-3.750 -0.0493 0.00786 0.00248 -0.0770 0.9003 0.0305
-3.500 -0.0230 0.00759 0.00216 -0.0764 0.8853 0.0356
-3.250 0.0037 0.00749 0.00200 -0.0760 0.8687 0.0394
-2.750 0.0545 0.00719 0.00162 -0.0745 0.8316 0.0580
-2.500 0.0794 0.00709 0.00149 -0.0737 0.8122 0.0727
-2.250 0.1041 0.00700 0.00138 -0.0728 0.7931 0.0921
-2.000 0.1287 0.00690 0.00129 -0.0719 0.7747 0.1174
-1.750 0.1532 0.00679 0.00121 -0.0711 0.7562 0.1490
-1.500 0.1774 0.00666 0.00115 -0.0702 0.7372 0.1922
-1.250 0.2012 0.00653 0.00110 -0.0692 0.7177 0.2446
-1.000 0.2251 0.00640 0.00107 -0.0683 0.6989 0.3026
-0.750 0.2487 0.00624 0.00105 -0.0673 0.6795 0.3729
-0.500 0.2720 0.00610 0.00104 -0.0663 0.6591 0.4491
-0.250 0.2952 0.00598 0.00105 -0.0652 0.6389 0.5246
0.000 0.3178 0.00583 0.00107 -0.0640 0.6191 0.6079
0.250 0.3370 0.00555 0.00110 -0.0619 0.6000 0.7345
0.500 0.4478 0.00526 0.00123 -0.0810 0.5657 0.9978
0.750 0.4799 0.00539 0.00125 -0.0819 0.5440 1.0000
1.000 0.5053 0.00552 0.00128 -0.0813 0.5242 1.0000
1.250 0.5307 0.00566 0.00131 -0.0807 0.5059 1.0000
1.500 0.5564 0.00578 0.00135 -0.0801 0.4885 1.0000
1.750 0.5822 0.00591 0.00140 -0.0795 0.4725 1.0000
2.000 0.6079 0.00604 0.00145 -0.0790 0.4572 1.0000
2.250 0.6336 0.00617 0.00152 -0.0784 0.4418 1.0000
2.500 0.6593 0.00631 0.00159 -0.0779 0.4278 1.0000
2.750 0.6850 0.00645 0.00166 -0.0774 0.4145 1.0000
3.000 0.7106 0.00659 0.00174 -0.0768 0.4004 1.0000
3.250 0.7362 0.00674 0.00184 -0.0763 0.3865 1.0000
3.500 0.7619 0.00689 0.00193 -0.0757 0.3737 1.0000
3.750 0.7875 0.00703 0.00204 -0.0752 0.3606 1.0000
4.000 0.8130 0.00720 0.00215 -0.0746 0.3470 1.0000
4.250 0.8384 0.00736 0.00227 -0.0741 0.3342 1.0000
4.500 0.8638 0.00753 0.00240 -0.0735 0.3219 1.0000
4.750 0.8890 0.00771 0.00254 -0.0730 0.3092 1.0000
5.000 0.9140 0.00791 0.00270 -0.0724 0.2955 1.0000
5.250 0.9390 0.00811 0.00286 -0.0717 0.2823 1.0000
5.500 0.9637 0.00834 0.00303 -0.0711 0.2683 1.0000
5.750 0.9879 0.00860 0.00322 -0.0704 0.2481 1.0000
6.000 1.0112 0.00894 0.00345 -0.0696 0.2257 1.0000
6.250 1.0351 0.00923 0.00367 -0.0688 0.2074 1.0000
6.500 1.0589 0.00954 0.00391 -0.0680 0.1905 1.0000
6.750 1.0827 0.00983 0.00415 -0.0673 0.1767 1.0000
7.000 1.1064 0.01014 0.00442 -0.0665 0.1637 1.0000
7.250 1.1298 0.01046 0.00469 -0.0657 0.1499 1.0000
7.500 1.1527 0.01083 0.00499 -0.0649 0.1348 1.0000
7.750 1.1750 0.01125 0.00533 -0.0639 0.1182 1.0000
8.000 1.1966 0.01173 0.00572 -0.0629 0.0983 1.0000
8.250 1.2148 0.01250 0.00629 -0.0613 0.0670 1.0000
8.500 1.2322 0.01335 0.00697 -0.0596 0.0408 1.0000
8.750 1.2513 0.01405 0.00759 -0.0582 0.0285 1.0000
9.000 1.2717 0.01460 0.00813 -0.0569 0.0229 1.0000
9.250 1.2920 0.01516 0.00872 -0.0557 0.0193 1.0000
9.500 1.3124 0.01569 0.00927 -0.0545 0.0171 1.0000
9.750 1.3302 0.01644 0.01007 -0.0529 0.0150 1.0000
10.000 1.3511 0.01689 0.01056 -0.0518 0.0143 1.0000
10.250 1.3709 0.01740 0.01112 -0.0505 0.0133 1.0000
10.500 1.3893 0.01800 0.01175 -0.0491 0.0124 1.0000
10.750 1.4033 0.01894 0.01278 -0.0470 0.0114 1.0000
11.000 1.4188 0.01970 0.01362 -0.0451 0.0110 1.0000
11.250 1.4358 0.02030 0.01428 -0.0436 0.0106 1.0000
11.500 1.4512 0.02098 0.01503 -0.0418 0.0102 1.0000
11.750 1.4642 0.02170 0.01581 -0.0396 0.0098 1.0000
12.000 1.4744 0.02243 0.01660 -0.0369 0.0094 1.0000
12.250 1.4836 0.02324 0.01747 -0.0343 0.0091 1.0000
12.500 1.4893 0.02431 0.01861 -0.0314 0.0087 1.0000
12.750 1.4864 0.02601 0.02043 -0.0279 0.0083 1.0000
13.000 1.4847 0.02780 0.02234 -0.0250 0.0081 1.0000
13.250 1.4937 0.02894 0.02357 -0.0235 0.0079 1.0000
13.500 1.4995 0.03041 0.02513 -0.0219 0.0077 1.0000
13.750 1.5032 0.03217 0.02699 -0.0205 0.0075 1.0000
14.000 1.5056 0.03420 0.02911 -0.0194 0.0074 1.0000
14.250 1.5068 0.03648 0.03150 -0.0186 0.0072 1.0000
14.500 1.5067 0.03907 0.03419 -0.0182 0.0070 1.0000
14.750 1.5056 0.04196 0.03718 -0.0181 0.0069 1.0000
15.000 1.5028 0.04519 0.04052 -0.0183 0.0067 1.0000
15.250 1.4987 0.04878 0.04421 -0.0189 0.0066 1.0000
15.500 1.4924 0.05279 0.04835 -0.0198 0.0065 1.0000
15.750 1.4839 0.05723 0.05289 -0.0210 0.0064 1.0000
16.000 1.4733 0.06212 0.05791 -0.0225 0.0063 1.0000
16.250 1.4604 0.06743 0.06333 -0.0242 0.0063 1.0000
16.500 1.4460 0.07313 0.06915 -0.0262 0.0062 1.0000
16.750 1.4304 0.07913 0.07527 -0.0284 0.0062 1.0000
17.000 1.4140 0.08534 0.08159 -0.0307 0.0061 1.0000
17.250 1.3973 0.09174 0.08810 -0.0331 0.0061 1.0000
17.500 1.3803 0.09827 0.09475 -0.0357 0.0060 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WASP (smoothed) (waspsm-il)