DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Reynolds number: 200,000 Max Cl/Cd: 60.1 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-defcnd1-il-200000-n5.txt Download as CSV file: xf-defcnd1-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: DEFIANT CANARD BL20 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-16.500 -0.5312 0.09163 0.08621 -0.0805 0.7832 0.0346
-16.250 -0.5394 0.08574 0.08014 -0.0850 0.7654 0.0355
-16.000 -0.5516 0.07975 0.07401 -0.0891 0.7542 0.0362
-15.750 -0.5651 0.07377 0.06786 -0.0932 0.7452 0.0368
-15.500 -0.5815 0.06800 0.06194 -0.0967 0.7375 0.0375
-15.250 -0.5974 0.06281 0.05659 -0.0996 0.7301 0.0381
-15.000 -0.6122 0.05808 0.05168 -0.1021 0.7235 0.0388
-14.750 -0.6259 0.05367 0.04716 -0.1043 0.7171 0.0394
-14.500 -0.6392 0.04951 0.04288 -0.1063 0.7107 0.0401
-14.250 -0.6498 0.04580 0.03902 -0.1079 0.7052 0.0410
-14.000 -0.6577 0.04246 0.03558 -0.1092 0.6993 0.0420
-13.750 -0.6627 0.03955 0.03252 -0.1102 0.6936 0.0434
-13.500 -0.6690 0.03672 0.02959 -0.1109 0.6885 0.0446
-13.250 -0.6728 0.03434 0.02710 -0.1111 0.6840 0.0461
-13.000 -0.6735 0.03239 0.02503 -0.1108 0.6789 0.0480
-12.750 -0.6757 0.03058 0.02317 -0.1100 0.6738 0.0499
-12.500 -0.6749 0.02916 0.02164 -0.1087 0.6690 0.0521
-12.000 -0.6690 0.02690 0.01921 -0.1052 0.6600 0.0571
-11.750 -0.6634 0.02599 0.01824 -0.1031 0.6554 0.0602
-11.500 -0.6563 0.02521 0.01739 -0.1009 0.6511 0.0636
-11.250 -0.6482 0.02454 0.01666 -0.0986 0.6472 0.0669
-11.000 -0.6382 0.02402 0.01603 -0.0962 0.6436 0.0709
-10.750 -0.6281 0.02356 0.01557 -0.0938 0.6393 0.0744
-10.500 -0.6144 0.02317 0.01510 -0.0918 0.6349 0.0787
-10.250 -0.5990 0.02281 0.01470 -0.0901 0.6307 0.0826
-10.000 -0.5814 0.02247 0.01425 -0.0886 0.6270 0.0869
-9.750 -0.5633 0.02219 0.01388 -0.0872 0.6238 0.0909
-9.500 -0.5435 0.02188 0.01349 -0.0859 0.6202 0.0950
-9.250 -0.5239 0.02161 0.01319 -0.0847 0.6162 0.0988
-9.000 -0.5026 0.02136 0.01281 -0.0837 0.6121 0.1031
-8.750 -0.4825 0.02110 0.01252 -0.0825 0.6084 0.1067
-8.500 -0.4608 0.02090 0.01220 -0.0815 0.6050 0.1111
-8.250 -0.4390 0.02066 0.01187 -0.0805 0.6020 0.1151
-8.000 -0.4171 0.02041 0.01162 -0.0796 0.5985 0.1189
-7.750 -0.3942 0.02018 0.01130 -0.0787 0.5947 0.1227
-7.500 -0.3714 0.01988 0.01094 -0.0779 0.5911 0.1259
-7.250 -0.3489 0.01956 0.01060 -0.0770 0.5876 0.1290
-7.000 -0.3254 0.01932 0.01027 -0.0762 0.5846 0.1324
-6.750 -0.3013 0.01911 0.00996 -0.0755 0.5816 0.1357
-6.500 -0.2779 0.01880 0.00965 -0.0747 0.5783 0.1387
-6.250 -0.2546 0.01851 0.00938 -0.0740 0.5748 0.1420
-6.000 -0.2305 0.01828 0.00911 -0.0733 0.5714 0.1454
-5.750 -0.2060 0.01807 0.00881 -0.0726 0.5681 0.1489
-5.500 -0.1820 0.01781 0.00851 -0.0719 0.5652 0.1523
-5.250 -0.1581 0.01758 0.00826 -0.0711 0.5625 0.1561
-5.000 -0.1337 0.01738 0.00807 -0.0705 0.5592 0.1603
-4.750 -0.1087 0.01722 0.00787 -0.0699 0.5559 0.1644
-4.500 -0.0850 0.01697 0.00765 -0.0691 0.5525 0.1691
-4.250 -0.0605 0.01677 0.00744 -0.0685 0.5494 0.1747
-4.000 -0.0353 0.01661 0.00722 -0.0679 0.5465 0.1807
-3.750 -0.0108 0.01642 0.00701 -0.0673 0.5440 0.1887
-3.500 0.0137 0.01626 0.00691 -0.0666 0.5410 0.1986
-3.250 0.0380 0.01608 0.00680 -0.0660 0.5377 0.2127
-3.000 0.0622 0.01589 0.00668 -0.0653 0.5344 0.2315
-2.750 0.0863 0.01569 0.00657 -0.0646 0.5312 0.2568
-2.500 0.1110 0.01552 0.00647 -0.0640 0.5284 0.2867
-2.250 0.1359 0.01540 0.00641 -0.0634 0.5259 0.3170
-2.000 0.1610 0.01536 0.00643 -0.0628 0.5232 0.3430
-1.750 0.1861 0.01534 0.00646 -0.0622 0.5198 0.3643
-1.500 0.2115 0.01532 0.00648 -0.0617 0.5164 0.3826
-1.250 0.2371 0.01529 0.00648 -0.0612 0.5132 0.3990
-1.000 0.2630 0.01529 0.00646 -0.0607 0.5104 0.4143
-0.750 0.2897 0.01530 0.00643 -0.0604 0.5080 0.4285
-0.500 0.3156 0.01533 0.00646 -0.0599 0.5052 0.4417
-0.250 0.3407 0.01537 0.00654 -0.0594 0.5018 0.4531
0.000 0.3661 0.01540 0.00659 -0.0589 0.4983 0.4653
0.250 0.3917 0.01541 0.00663 -0.0584 0.4953 0.4772
0.500 0.4175 0.01542 0.00664 -0.0579 0.4925 0.4925
0.750 0.4432 0.01542 0.00663 -0.0574 0.4899 0.5097
1.000 0.4682 0.01543 0.00669 -0.0569 0.4871 0.5254
1.250 0.4920 0.01545 0.00681 -0.0561 0.4836 0.5411
1.500 0.5161 0.01547 0.00691 -0.0554 0.4803 0.5584
2.000 0.5645 0.01543 0.00701 -0.0539 0.4743 0.5990
2.250 0.5892 0.01539 0.00703 -0.0532 0.4716 0.6244
2.500 0.6120 0.01539 0.00717 -0.0522 0.4687 0.6573
2.750 0.6335 0.01537 0.00738 -0.0510 0.4654 0.7024
3.000 0.6579 0.01534 0.00759 -0.0501 0.4619 0.7636
3.250 0.6958 0.01538 0.00781 -0.0520 0.4584 0.8381
3.500 0.7505 0.01554 0.00799 -0.0572 0.4551 0.8944
3.750 0.7983 0.01575 0.00817 -0.0612 0.4520 0.9279
4.000 0.8404 0.01601 0.00848 -0.0643 0.4478 0.9501
4.250 0.8786 0.01624 0.00871 -0.0666 0.4438 0.9666
4.500 0.9149 0.01644 0.00888 -0.0685 0.4404 0.9804
4.750 0.9541 0.01663 0.00899 -0.0710 0.4373 0.9914
5.000 0.9946 0.01687 0.00919 -0.0739 0.4339 1.0000
5.250 1.0090 0.01710 0.00947 -0.0717 0.4302 1.0000
5.500 1.0245 0.01732 0.00969 -0.0696 0.4267 1.0000
5.750 1.0410 0.01752 0.00987 -0.0678 0.4236 1.0000
6.000 1.0588 0.01770 0.01000 -0.0661 0.4206 1.0000
6.250 1.0764 0.01791 0.01016 -0.0644 0.4176 1.0000
6.500 1.0886 0.01822 0.01054 -0.0619 0.4139 1.0000
6.750 1.1019 0.01851 0.01085 -0.0595 0.4103 1.0000
7.000 1.1161 0.01878 0.01110 -0.0573 0.4069 1.0000
7.250 1.1318 0.01902 0.01130 -0.0554 0.4039 1.0000
7.500 1.1469 0.01928 0.01152 -0.0533 0.4008 1.0000
7.750 1.1503 0.01968 0.01200 -0.0494 0.3971 1.0000
8.000 1.1569 0.02008 0.01244 -0.0461 0.3935 1.0000
8.250 1.1670 0.02047 0.01283 -0.0435 0.3902 1.0000
8.500 1.1805 0.02082 0.01314 -0.0415 0.3870 1.0000
8.750 1.1935 0.02124 0.01354 -0.0396 0.3838 1.0000
9.000 1.1970 0.02199 0.01439 -0.0367 0.3797 1.0000
9.250 1.2042 0.02271 0.01515 -0.0345 0.3758 1.0000
9.500 1.2155 0.02333 0.01577 -0.0328 0.3723 1.0000
9.750 1.2312 0.02381 0.01620 -0.0316 0.3691 1.0000
10.000 1.2351 0.02491 0.01739 -0.0296 0.3651 1.0000
10.250 1.2378 0.02618 0.01874 -0.0278 0.3606 1.0000
10.500 1.2468 0.02719 0.01976 -0.0266 0.3568 1.0000
10.750 1.2613 0.02788 0.02043 -0.0257 0.3536 1.0000
11.000 1.2678 0.02916 0.02174 -0.0245 0.3498 1.0000
11.250 1.2662 0.03105 0.02375 -0.0231 0.3449 1.0000
11.500 1.2731 0.03239 0.02511 -0.0222 0.3407 1.0000
11.750 1.2879 0.03313 0.02582 -0.0215 0.3374 1.0000
12.000 1.2921 0.03475 0.02748 -0.0206 0.3336 1.0000
12.250 1.2874 0.03713 0.02998 -0.0195 0.3287 1.0000
12.500 1.2935 0.03864 0.03151 -0.0188 0.3245 1.0000
12.750 1.3094 0.03932 0.03215 -0.0182 0.3213 1.0000
13.000 1.3086 0.04150 0.03441 -0.0175 0.3171 1.0000
13.250 1.3021 0.04427 0.03728 -0.0167 0.3123 1.0000
13.500 1.3092 0.04581 0.03884 -0.0162 0.3083 1.0000
13.750 1.3273 0.04633 0.03932 -0.0158 0.3053 1.0000
14.000 1.3198 0.04938 0.04248 -0.0153 0.3007 1.0000
14.250 1.3127 0.05248 0.04568 -0.0149 0.2959 1.0000
14.500 1.3222 0.05392 0.04714 -0.0146 0.2923 1.0000
14.750 1.3428 0.05419 0.04735 -0.0143 0.2895 1.0000
15.000 1.3254 0.05855 0.05186 -0.0141 0.2842 1.0000
15.250 1.3195 0.06176 0.05517 -0.0140 0.2797 1.0000
15.500 1.3320 0.06292 0.05633 -0.0138 0.2765 1.0000
15.750 1.3547 0.06293 0.05630 -0.0135 0.2741 1.0000
16.000 1.3275 0.06869 0.06224 -0.0138 0.2684 1.0000
16.250 1.3215 0.07209 0.06571 -0.0139 0.2637 1.0000
16.500 1.3373 0.07290 0.06652 -0.0138 0.2610 1.0000
16.750 1.3641 0.07235 0.06592 -0.0135 0.2586 1.0000
17.000 1.3148 0.08113 0.07494 -0.0144 0.2513 1.0000
17.250 1.3203 0.08323 0.07707 -0.0146 0.2474 1.0000
17.500 1.3459 0.08278 0.07657 -0.0144 0.2447 1.0000
17.750 1.3069 0.09060 0.08457 -0.0155 0.2379 1.0000
18.000 1.3041 0.09385 0.08787 -0.0160 0.2331 1.0000
18.250 1.3323 0.09298 0.08694 -0.0158 0.2303 1.0000
18.500 1.2892 0.10168 0.09583 -0.0174 0.2234 1.0000
18.750 1.2901 0.10450 0.09869 -0.0180 0.2187 1.0000
19.000 1.3182 0.10355 0.09769 -0.0178 0.2160 1.0000
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