DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: DEFIANT CANARD BL20 AIRFOIL (defcnd1-il) Reynolds number: 1,000,000 Max Cl/Cd: 124.87 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-defcnd1-il-1000000.txt Download as CSV file: xf-defcnd1-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7574 0.11293 0.10986 -0.0467 1.0000 0.0180
-18.750 -0.7665 0.10782 0.10469 -0.0494 1.0000 0.0181
-18.500 -0.7740 0.10135 0.09816 -0.0540 0.9549 0.0183
-18.250 -0.7576 0.08993 0.08651 -0.0715 0.9154 0.0186
-18.000 -0.7368 0.07699 0.07314 -0.0932 0.8582 0.0190
-17.750 -0.7489 0.06985 0.06546 -0.1003 0.7626 0.0195
-17.500 -0.7706 0.06377 0.05918 -0.1038 0.7437 0.0195
-17.250 -0.7904 0.05824 0.05349 -0.1068 0.7316 0.0196
-17.000 -0.8100 0.05309 0.04818 -0.1095 0.7220 0.0196
-16.750 -0.8263 0.04858 0.04355 -0.1116 0.7140 0.0198
-16.500 -0.8393 0.04458 0.03942 -0.1133 0.7060 0.0199
-16.250 -0.8484 0.04107 0.03582 -0.1146 0.7000 0.0202
-16.000 -0.8565 0.03776 0.03239 -0.1158 0.6935 0.0204
-15.750 -0.8611 0.03489 0.02940 -0.1166 0.6866 0.0207
-15.500 -0.8629 0.03229 0.02671 -0.1173 0.6816 0.0209
-15.250 -0.8657 0.02976 0.02409 -0.1177 0.6760 0.0211
-15.000 -0.8735 0.02714 0.02137 -0.1176 0.6707 0.0216
-14.750 -0.8757 0.02529 0.01942 -0.1168 0.6644 0.0220
-14.500 -0.8760 0.02372 0.01780 -0.1155 0.6606 0.0224
-14.250 -0.8734 0.02251 0.01653 -0.1139 0.6560 0.0229
-14.000 -0.8690 0.02153 0.01548 -0.1120 0.6513 0.0233
-13.750 -0.8626 0.02075 0.01461 -0.1099 0.6462 0.0239
-13.500 -0.8583 0.01991 0.01371 -0.1074 0.6420 0.0246
-13.250 -0.8527 0.01914 0.01292 -0.1048 0.6384 0.0253
-13.000 -0.8453 0.01850 0.01223 -0.1021 0.6341 0.0263
-12.750 -0.8353 0.01799 0.01166 -0.0996 0.6298 0.0272
-12.500 -0.8272 0.01744 0.01106 -0.0967 0.6252 0.0284
-12.250 -0.8180 0.01694 0.01054 -0.0938 0.6218 0.0297
-12.000 -0.8069 0.01655 0.01012 -0.0910 0.6188 0.0314
-11.750 -0.7953 0.01610 0.00966 -0.0884 0.6152 0.0336
-11.500 -0.7799 0.01565 0.00919 -0.0864 0.6114 0.0366
-11.250 -0.7634 0.01524 0.00876 -0.0846 0.6072 0.0402
-11.000 -0.7456 0.01487 0.00836 -0.0829 0.6026 0.0440
-10.750 -0.7263 0.01447 0.00797 -0.0815 0.6001 0.0485
-10.500 -0.7064 0.01408 0.00760 -0.0802 0.5972 0.0531
-10.250 -0.6858 0.01372 0.00725 -0.0789 0.5938 0.0580
-10.000 -0.6645 0.01340 0.00693 -0.0777 0.5902 0.0629
-9.750 -0.6426 0.01312 0.00664 -0.0766 0.5862 0.0680
-9.500 -0.6197 0.01289 0.00640 -0.0757 0.5822 0.0730
-9.250 -0.5953 0.01266 0.00618 -0.0750 0.5797 0.0785
-9.000 -0.5709 0.01243 0.00598 -0.0743 0.5767 0.0837
-8.750 -0.5456 0.01226 0.00581 -0.0737 0.5736 0.0879
-8.500 -0.5202 0.01212 0.00565 -0.0731 0.5702 0.0920
-8.250 -0.4943 0.01202 0.00550 -0.0726 0.5664 0.0952
-8.000 -0.4690 0.01188 0.00536 -0.0720 0.5626 0.0988
-7.750 -0.4420 0.01177 0.00524 -0.0717 0.5602 0.1019
-7.500 -0.4152 0.01165 0.00510 -0.0713 0.5574 0.1044
-7.250 -0.3895 0.01148 0.00494 -0.0708 0.5544 0.1076
-7.000 -0.3628 0.01139 0.00483 -0.0704 0.5512 0.1104
-6.750 -0.3359 0.01133 0.00472 -0.0701 0.5477 0.1125
-6.500 -0.3096 0.01125 0.00459 -0.0696 0.5437 0.1149
-6.250 -0.2833 0.01107 0.00444 -0.0692 0.5415 0.1186
-6.000 -0.2558 0.01098 0.00436 -0.0690 0.5390 0.1218
-5.750 -0.2281 0.01091 0.00427 -0.0688 0.5362 0.1240
-5.500 -0.2016 0.01079 0.00411 -0.0684 0.5332 0.1262
-5.250 -0.1759 0.01063 0.00393 -0.0678 0.5299 0.1293
-5.000 -0.1496 0.01056 0.00383 -0.0674 0.5258 0.1320
-4.750 -0.1222 0.01045 0.00372 -0.0671 0.5235 0.1343
-4.500 -0.0945 0.01037 0.00362 -0.0669 0.5212 0.1363
-4.250 -0.0675 0.01024 0.00349 -0.0666 0.5186 0.1391
-4.000 -0.0408 0.01010 0.00336 -0.0663 0.5157 0.1430
-3.750 -0.0139 0.01001 0.00325 -0.0659 0.5125 0.1466
-3.500 0.0132 0.00998 0.00318 -0.0656 0.5090 0.1497
-3.250 0.0398 0.00989 0.00308 -0.0653 0.5059 0.1551
-3.000 0.0672 0.00976 0.00300 -0.0650 0.5039 0.1615
-2.750 0.0943 0.00963 0.00291 -0.0648 0.5013 0.1707
-2.500 0.1210 0.00948 0.00281 -0.0644 0.4984 0.1857
-2.000 0.1714 0.00907 0.00264 -0.0634 0.4924 0.2548
-1.750 0.1964 0.00894 0.00261 -0.0628 0.4885 0.2939
-1.500 0.2233 0.00880 0.00259 -0.0625 0.4866 0.3234
-1.250 0.2507 0.00871 0.00257 -0.0623 0.4841 0.3459
-1.000 0.2782 0.00866 0.00256 -0.0621 0.4814 0.3641
-0.750 0.3054 0.00862 0.00256 -0.0619 0.4786 0.3804
-0.500 0.3325 0.00861 0.00256 -0.0616 0.4754 0.3939
-0.250 0.3595 0.00866 0.00259 -0.0613 0.4716 0.4058
0.000 0.3869 0.00864 0.00262 -0.0611 0.4692 0.4186
0.250 0.4150 0.00864 0.00263 -0.0611 0.4669 0.4284
0.500 0.4426 0.00862 0.00265 -0.0609 0.4642 0.4391
0.750 0.4704 0.00864 0.00267 -0.0608 0.4612 0.4475
1.000 0.4970 0.00865 0.00269 -0.0605 0.4580 0.4578
1.250 0.5236 0.00872 0.00274 -0.0602 0.4544 0.4669
1.500 0.5506 0.00874 0.00279 -0.0599 0.4517 0.4774
1.750 0.5783 0.00874 0.00282 -0.0598 0.4493 0.4896
2.000 0.6052 0.00872 0.00286 -0.0596 0.4464 0.5028
2.250 0.6322 0.00876 0.00290 -0.0594 0.4434 0.5135
2.500 0.6579 0.00878 0.00295 -0.0589 0.4402 0.5265
2.750 0.6829 0.00884 0.00302 -0.0584 0.4364 0.5409
3.000 0.7091 0.00883 0.00308 -0.0580 0.4339 0.5593
3.250 0.7347 0.00878 0.00313 -0.0575 0.4313 0.5848
3.500 0.7586 0.00870 0.00320 -0.0567 0.4285 0.6288
3.750 0.7788 0.00855 0.00328 -0.0552 0.4254 0.7071
4.000 0.7956 0.00839 0.00339 -0.0529 0.4220 0.8019
4.250 0.8175 0.00833 0.00357 -0.0515 0.4182 0.8893
4.500 0.8712 0.00841 0.00377 -0.0569 0.4155 0.9395
4.750 0.9250 0.00856 0.00393 -0.0624 0.4118 0.9565
5.000 0.9674 0.00873 0.00407 -0.0655 0.4078 0.9668
5.250 1.0009 0.00895 0.00424 -0.0668 0.4037 0.9762
5.500 1.0377 0.00912 0.00441 -0.0688 0.4003 0.9813
5.750 1.0766 0.00925 0.00453 -0.0712 0.3972 0.9857
6.000 1.1126 0.00941 0.00468 -0.0730 0.3933 0.9904
6.250 1.1489 0.00960 0.00484 -0.0750 0.3893 0.9937
6.500 1.1859 0.00983 0.00503 -0.0772 0.3847 0.9967
6.750 1.2257 0.00993 0.00515 -0.0799 0.3817 0.9989
7.000 1.2574 0.01007 0.00529 -0.0809 0.3779 1.0000
7.250 1.2738 0.01022 0.00543 -0.0789 0.3743 1.0000
7.500 1.2880 0.01043 0.00561 -0.0764 0.3705 1.0000
7.750 1.3038 0.01060 0.00579 -0.0743 0.3673 1.0000
8.000 1.3218 0.01072 0.00593 -0.0725 0.3643 1.0000
8.250 1.3378 0.01089 0.00610 -0.0704 0.3607 1.0000
8.500 1.3509 0.01111 0.00631 -0.0678 0.3570 1.0000
8.750 1.3555 0.01136 0.00654 -0.0635 0.3531 1.0000
9.000 1.3687 0.01153 0.00674 -0.0609 0.3503 1.0000
9.250 1.3836 0.01172 0.00694 -0.0587 0.3469 1.0000
9.500 1.3971 0.01197 0.00721 -0.0564 0.3432 1.0000
9.750 1.4082 0.01234 0.00756 -0.0538 0.3392 1.0000
10.000 1.4201 0.01274 0.00797 -0.0515 0.3354 1.0000
10.250 1.4380 0.01302 0.00828 -0.0502 0.3325 1.0000
10.500 1.4530 0.01341 0.00868 -0.0486 0.3286 1.0000
10.750 1.4651 0.01395 0.00923 -0.0467 0.3247 1.0000
11.000 1.4733 0.01471 0.00998 -0.0445 0.3203 1.0000
11.250 1.4907 0.01517 0.01048 -0.0436 0.3175 1.0000
11.500 1.5052 0.01579 0.01113 -0.0424 0.3139 1.0000
11.750 1.5161 0.01666 0.01202 -0.0411 0.3098 1.0000
12.000 1.5223 0.01792 0.01327 -0.0396 0.3052 1.0000
12.250 1.5367 0.01877 0.01417 -0.0390 0.3016 1.0000
12.500 1.5485 0.01986 0.01529 -0.0383 0.2972 1.0000
12.750 1.5553 0.02133 0.01677 -0.0373 0.2929 1.0000
13.000 1.5596 0.02300 0.01844 -0.0363 0.2880 1.0000
13.250 1.5716 0.02412 0.01962 -0.0358 0.2847 1.0000
13.500 1.5781 0.02565 0.02117 -0.0350 0.2804 1.0000
13.750 1.5786 0.02761 0.02314 -0.0339 0.2761 1.0000
14.000 1.5831 0.02928 0.02484 -0.0330 0.2719 1.0000
14.250 1.5900 0.03080 0.02641 -0.0323 0.2682 1.0000
14.500 1.5922 0.03268 0.02830 -0.0314 0.2642 1.0000
14.750 1.5865 0.03521 0.03083 -0.0303 0.2590 1.0000
15.000 1.5935 0.03683 0.03251 -0.0298 0.2558 1.0000
15.250 1.5996 0.03851 0.03422 -0.0293 0.2522 1.0000
15.500 1.5972 0.04098 0.03671 -0.0286 0.2477 1.0000
15.750 1.5947 0.04348 0.03921 -0.0279 0.2434 1.0000
16.000 1.6019 0.04520 0.04099 -0.0276 0.2401 1.0000
16.250 1.6046 0.04729 0.04310 -0.0272 0.2356 1.0000
16.500 1.5981 0.05030 0.04612 -0.0266 0.2310 1.0000
16.750 1.6017 0.05238 0.04823 -0.0263 0.2266 1.0000
17.000 1.6028 0.05474 0.05064 -0.0261 0.2226 1.0000
17.250 1.5999 0.05746 0.05335 -0.0257 0.2181 1.0000
17.500 1.5964 0.06034 0.05627 -0.0255 0.2141 1.0000
17.750 1.6018 0.06231 0.05828 -0.0254 0.2107 1.0000
18.000 1.6004 0.06501 0.06101 -0.0253 0.2067 1.0000
18.250 1.5926 0.06837 0.06437 -0.0252 0.2018 1.0000
18.500 1.5964 0.07057 0.06663 -0.0252 0.1986 1.0000
18.750 1.5959 0.07327 0.06936 -0.0252 0.1947 1.0000
19.000 1.5913 0.07638 0.07248 -0.0253 0.1902 1.0000
19.250 1.5867 0.07955 0.07569 -0.0254 0.1863 1.0000
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