DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Reynolds number: 1,000,000 Max Cl/Cd: 116.6 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-defcnd1-il-1000000-n5.txt Download as CSV file: xf-defcnd1-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.6991 0.08681 0.08216 -0.0914 0.6765 0.0149
-18.250 -0.7350 0.07836 0.07357 -0.0960 0.6750 0.0147
-18.000 -0.7668 0.07077 0.06583 -0.1002 0.6712 0.0148
-17.750 -0.7889 0.06474 0.05967 -0.1035 0.6675 0.0151
-17.500 -0.8121 0.05885 0.05364 -0.1066 0.6641 0.0151
-17.250 -0.8311 0.05377 0.04846 -0.1091 0.6609 0.0151
-17.000 -0.8470 0.04931 0.04389 -0.1111 0.6568 0.0151
-16.750 -0.8598 0.04532 0.03980 -0.1128 0.6527 0.0152
-16.500 -0.8686 0.04188 0.03625 -0.1141 0.6482 0.0153
-16.000 -0.8841 0.03539 0.02958 -0.1162 0.6410 0.0157
-15.750 -0.8887 0.03255 0.02665 -0.1169 0.6373 0.0159
-15.500 -0.8908 0.03009 0.02411 -0.1173 0.6334 0.0162
-15.250 -0.8909 0.02803 0.02197 -0.1173 0.6288 0.0163
-15.000 -0.8903 0.02624 0.02010 -0.1167 0.6247 0.0166
-14.750 -0.8880 0.02475 0.01854 -0.1158 0.6209 0.0169
-14.500 -0.8846 0.02347 0.01721 -0.1145 0.6172 0.0172
-14.250 -0.8796 0.02242 0.01609 -0.1130 0.6134 0.0175
-14.000 -0.8737 0.02152 0.01512 -0.1111 0.6096 0.0178
-13.750 -0.8667 0.02074 0.01428 -0.1091 0.6057 0.0181
-13.500 -0.8604 0.01999 0.01348 -0.1068 0.6020 0.0186
-13.250 -0.8521 0.01933 0.01278 -0.1045 0.5990 0.0190
-13.000 -0.8432 0.01873 0.01215 -0.1020 0.5953 0.0196
-12.750 -0.8328 0.01822 0.01159 -0.0996 0.5915 0.0202
-12.500 -0.8215 0.01776 0.01108 -0.0971 0.5878 0.0209
-12.250 -0.8106 0.01731 0.01059 -0.0945 0.5843 0.0215
-12.000 -0.7997 0.01691 0.01015 -0.0918 0.5815 0.0224
-11.750 -0.7872 0.01656 0.00979 -0.0892 0.5789 0.0235
-11.500 -0.7711 0.01618 0.00938 -0.0873 0.5756 0.0248
-11.250 -0.7539 0.01579 0.00897 -0.0856 0.5719 0.0266
-11.000 -0.7353 0.01545 0.00859 -0.0841 0.5683 0.0282
-10.750 -0.7163 0.01511 0.00822 -0.0826 0.5645 0.0302
-10.500 -0.6964 0.01475 0.00786 -0.0813 0.5619 0.0326
-10.250 -0.6757 0.01441 0.00751 -0.0800 0.5594 0.0357
-10.000 -0.6544 0.01409 0.00718 -0.0789 0.5564 0.0389
-9.750 -0.6329 0.01376 0.00685 -0.0777 0.5531 0.0424
-9.500 -0.6109 0.01346 0.00655 -0.0767 0.5495 0.0461
-9.250 -0.5888 0.01316 0.00624 -0.0756 0.5458 0.0510
-9.000 -0.5659 0.01288 0.00596 -0.0747 0.5430 0.0555
-8.750 -0.5422 0.01261 0.00570 -0.0739 0.5408 0.0603
-8.500 -0.5182 0.01236 0.00546 -0.0731 0.5380 0.0653
-8.250 -0.4939 0.01213 0.00524 -0.0724 0.5350 0.0710
-8.000 -0.4693 0.01192 0.00504 -0.0717 0.5315 0.0764
-7.750 -0.4442 0.01174 0.00486 -0.0711 0.5280 0.0814
-7.500 -0.4184 0.01161 0.00471 -0.0706 0.5248 0.0858
-7.250 -0.3923 0.01144 0.00456 -0.0701 0.5227 0.0897
-7.000 -0.3657 0.01132 0.00443 -0.0697 0.5202 0.0934
-6.750 -0.3392 0.01119 0.00429 -0.0693 0.5172 0.0961
-6.500 -0.3128 0.01107 0.00416 -0.0689 0.5139 0.0996
-6.250 -0.2859 0.01099 0.00405 -0.0686 0.5105 0.1030
-6.000 -0.2596 0.01088 0.00393 -0.0681 0.5072 0.1068
-5.750 -0.2326 0.01077 0.00383 -0.0678 0.5051 0.1098
-5.500 -0.2052 0.01068 0.00372 -0.0676 0.5028 0.1119
-5.250 -0.1777 0.01060 0.00362 -0.0673 0.5000 0.1135
-5.000 -0.1509 0.01049 0.00350 -0.0670 0.4967 0.1161
-4.750 -0.1240 0.01040 0.00340 -0.0667 0.4935 0.1184
-4.500 -0.0970 0.01033 0.00330 -0.0663 0.4904 0.1207
-4.250 -0.0697 0.01027 0.00322 -0.0661 0.4878 0.1228
-4.000 -0.0418 0.01020 0.00314 -0.0659 0.4857 0.1245
-3.750 -0.0145 0.01011 0.00305 -0.0657 0.4829 0.1277
-3.500 0.0127 0.01002 0.00297 -0.0654 0.4799 0.1306
-3.250 0.0401 0.00996 0.00289 -0.0651 0.4768 0.1334
-3.000 0.0674 0.00992 0.00283 -0.0649 0.4738 0.1361
-2.750 0.0945 0.00988 0.00277 -0.0646 0.4706 0.1397
-2.500 0.1220 0.00979 0.00271 -0.0644 0.4684 0.1441
-2.250 0.1497 0.00973 0.00266 -0.0643 0.4658 0.1489
-2.000 0.1769 0.00965 0.00260 -0.0640 0.4629 0.1565
-1.750 0.2040 0.00958 0.00256 -0.0638 0.4600 0.1664
-1.500 0.2305 0.00950 0.00251 -0.0634 0.4568 0.1809
-1.250 0.2565 0.00940 0.00247 -0.0630 0.4534 0.2010
-1.000 0.2830 0.00927 0.00243 -0.0627 0.4511 0.2273
-0.750 0.3095 0.00914 0.00240 -0.0624 0.4488 0.2549
-0.500 0.3360 0.00904 0.00238 -0.0620 0.4458 0.2819
-0.250 0.3625 0.00897 0.00237 -0.0617 0.4426 0.3060
0.000 0.3889 0.00893 0.00238 -0.0614 0.4393 0.3276
0.250 0.4154 0.00893 0.00241 -0.0610 0.4361 0.3443
0.500 0.4427 0.00890 0.00243 -0.0608 0.4338 0.3593
0.750 0.4700 0.00889 0.00245 -0.0607 0.4312 0.3714
1.000 0.4973 0.00890 0.00248 -0.0605 0.4280 0.3831
1.250 0.5241 0.00891 0.00252 -0.0602 0.4248 0.3942
1.500 0.5508 0.00896 0.00256 -0.0599 0.4216 0.4059
1.750 0.5768 0.00898 0.00262 -0.0595 0.4181 0.4221
2.000 0.6038 0.00898 0.00267 -0.0593 0.4156 0.4361
2.250 0.6309 0.00901 0.00272 -0.0591 0.4127 0.4464
2.500 0.6573 0.00904 0.00278 -0.0588 0.4095 0.4567
2.750 0.6834 0.00910 0.00285 -0.0584 0.4061 0.4679
3.000 0.7086 0.00917 0.00293 -0.0579 0.4024 0.4796
3.250 0.7351 0.00921 0.00300 -0.0576 0.3996 0.4901
3.500 0.7611 0.00924 0.00307 -0.0573 0.3969 0.5023
3.750 0.7868 0.00928 0.00314 -0.0569 0.3936 0.5154
4.000 0.8116 0.00934 0.00323 -0.0563 0.3898 0.5287
4.250 0.8355 0.00943 0.00333 -0.0556 0.3859 0.5418
4.500 0.8603 0.00947 0.00343 -0.0550 0.3832 0.5580
4.750 0.8846 0.00949 0.00352 -0.0544 0.3803 0.5803
5.000 0.9072 0.00949 0.00363 -0.0534 0.3768 0.6186
5.250 0.9268 0.00945 0.00376 -0.0519 0.3729 0.6779
5.500 0.9439 0.00943 0.00391 -0.0498 0.3691 0.7449
5.750 0.9611 0.00934 0.00405 -0.0477 0.3666 0.8166
6.000 0.9849 0.00928 0.00423 -0.0468 0.3635 0.8989
6.250 1.0525 0.00952 0.00454 -0.0554 0.3582 0.9480
6.500 1.1046 0.00981 0.00480 -0.0609 0.3530 0.9623
6.750 1.1457 0.01001 0.00500 -0.0639 0.3496 0.9712
7.000 1.1777 0.01020 0.00519 -0.0650 0.3455 0.9798
7.250 1.2089 0.01044 0.00541 -0.0660 0.3410 0.9864
7.500 1.2354 0.01072 0.00566 -0.0661 0.3369 0.9944
8.000 1.3012 0.01116 0.00611 -0.0689 0.3298 1.0000
8.250 1.3119 0.01137 0.00631 -0.0658 0.3261 1.0000
8.500 1.3175 0.01160 0.00653 -0.0618 0.3223 1.0000
8.750 1.3275 0.01185 0.00678 -0.0587 0.3190 1.0000
9.000 1.3417 0.01207 0.00702 -0.0564 0.3162 1.0000
9.250 1.3553 0.01236 0.00732 -0.0542 0.3125 1.0000
9.500 1.3677 0.01273 0.00768 -0.0519 0.3086 1.0000
9.750 1.3782 0.01321 0.00816 -0.0494 0.3043 1.0000
10.000 1.3941 0.01358 0.00855 -0.0479 0.3017 1.0000
10.250 1.4089 0.01402 0.00901 -0.0464 0.2985 1.0000
10.500 1.4213 0.01461 0.00961 -0.0447 0.2944 1.0000
10.750 1.4315 0.01537 0.01038 -0.0429 0.2906 1.0000
11.000 1.4441 0.01611 0.01114 -0.0416 0.2874 1.0000
11.250 1.4580 0.01686 0.01192 -0.0406 0.2843 1.0000
11.500 1.4700 0.01780 0.01288 -0.0396 0.2807 1.0000
11.750 1.4787 0.01905 0.01414 -0.0386 0.2767 1.0000
12.000 1.4870 0.02041 0.01553 -0.0377 0.2729 1.0000
12.250 1.4986 0.02157 0.01672 -0.0371 0.2690 1.0000
12.500 1.5065 0.02302 0.01819 -0.0363 0.2646 1.0000
12.750 1.5087 0.02488 0.02007 -0.0352 0.2600 1.0000
13.000 1.5156 0.02639 0.02160 -0.0344 0.2558 1.0000
13.250 1.5223 0.02793 0.02317 -0.0336 0.2522 1.0000
13.500 1.5219 0.03001 0.02526 -0.0326 0.2471 1.0000
13.750 1.5222 0.03206 0.02733 -0.0316 0.2435 1.0000
14.000 1.5282 0.03366 0.02897 -0.0309 0.2396 1.0000
14.250 1.5302 0.03564 0.03098 -0.0301 0.2355 1.0000
14.500 1.5294 0.03789 0.03325 -0.0293 0.2312 1.0000
14.750 1.5301 0.04010 0.03548 -0.0286 0.2273 1.0000
15.000 1.5351 0.04195 0.03736 -0.0281 0.2232 1.0000
15.250 1.5342 0.04440 0.03984 -0.0276 0.2190 1.0000
15.500 1.5309 0.04707 0.04252 -0.0270 0.2141 1.0000
15.750 1.5348 0.04911 0.04459 -0.0266 0.2104 1.0000
16.000 1.5364 0.05139 0.04690 -0.0263 0.2062 1.0000
16.250 1.5298 0.05451 0.05003 -0.0258 0.2015 1.0000
16.500 1.5348 0.05650 0.05205 -0.0256 0.1979 1.0000
16.750 1.5303 0.05949 0.05506 -0.0253 0.1921 1.0000
17.000 1.5257 0.06251 0.05809 -0.0251 0.1872 1.0000
17.250 1.5257 0.06511 0.06072 -0.0250 0.1828 1.0000
17.500 1.5211 0.06818 0.06380 -0.0249 0.1771 1.0000
17.750 1.5168 0.07129 0.06693 -0.0249 0.1732 1.0000
18.000 1.5184 0.07378 0.06945 -0.0249 0.1687 1.0000
18.250 1.5115 0.07725 0.07294 -0.0250 0.1642 1.0000
18.500 1.5103 0.08007 0.07578 -0.0251 0.1602 1.0000
18.750 1.5077 0.08311 0.07886 -0.0253 0.1560 1.0000
19.000 1.4989 0.08689 0.08264 -0.0256 0.1504 1.0000
19.250 1.4966 0.08995 0.08574 -0.0259 0.1458 1.0000
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