WACO COOTIE AIRFOIL (cootie-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WACO COOTIE AIRFOIL (cootie-il) Reynolds number: 500,000 Max Cl/Cd: 116.02 at α=4° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-cootie-il-500000.txt Download as CSV file: xf-cootie-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WACO COOTIE AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.2876 0.10232 0.10013 -0.0334 1.0000 0.0187
-9.250 -0.2843 0.09986 0.09770 -0.0337 1.0000 0.0191
-9.000 -0.2803 0.09730 0.09518 -0.0347 0.9980 0.0196
-8.750 -0.2632 0.09329 0.09116 -0.0395 0.9934 0.0207
-8.500 -0.2462 0.08886 0.08673 -0.0499 0.9800 0.0220
-8.250 -0.2266 0.08417 0.08202 -0.0581 0.9696 0.0221
-8.000 -0.2083 0.07967 0.07750 -0.0643 0.9586 0.0222
-7.750 -0.2007 0.07453 0.07235 -0.0663 0.9490 0.0226
-7.500 -0.1877 0.07198 0.06977 -0.0663 0.9409 0.0230
-7.250 -0.1735 0.06934 0.06710 -0.0679 0.9314 0.0235
-7.000 -0.1571 0.06642 0.06412 -0.0708 0.9229 0.0242
-6.750 -0.1385 0.06318 0.06081 -0.0745 0.9146 0.0253
-6.500 -0.0994 0.05816 0.05564 -0.0858 0.9061 0.0281
-6.250 -0.0730 0.05380 0.05115 -0.0907 0.8991 0.0283
-6.000 -0.0589 0.04826 0.04554 -0.0936 0.8922 0.0292
-5.750 -0.0389 0.04626 0.04348 -0.0944 0.8855 0.0299
-5.500 -0.0157 0.04402 0.04116 -0.0960 0.8792 0.0309
-5.250 0.0116 0.04121 0.03823 -0.0986 0.8722 0.0334
-5.000 0.0501 0.03428 0.03087 -0.1047 0.8666 0.0372
-4.750 0.0729 0.03278 0.02933 -0.1051 0.8593 0.0381
-4.500 0.0975 0.03135 0.02779 -0.1056 0.8529 0.0395
-4.250 0.1256 0.02928 0.02558 -0.1067 0.8456 0.0426
-4.000 0.1561 0.02584 0.02178 -0.1082 0.8389 0.0479
-3.750 0.1818 0.02487 0.02075 -0.1085 0.8306 0.0498
-3.500 0.2129 0.02246 0.01788 -0.1091 0.8225 0.0578
-3.250 0.2386 0.02133 0.01673 -0.1093 0.8114 0.0592
-3.000 0.2719 0.01481 0.00929 -0.1097 0.8027 0.0432
-2.750 0.3007 0.01223 0.00617 -0.1096 0.7925 0.0401
-2.500 0.3289 0.01139 0.00515 -0.1095 0.7808 0.0399
-2.250 0.3570 0.01080 0.00442 -0.1094 0.7696 0.0400
-2.000 0.3850 0.01034 0.00385 -0.1093 0.7580 0.0403
-1.750 0.4128 0.01001 0.00344 -0.1092 0.7450 0.0412
-1.500 0.4407 0.00972 0.00306 -0.1091 0.7313 0.0421
-1.250 0.4686 0.00947 0.00273 -0.1091 0.7174 0.0426
-1.000 0.4965 0.00929 0.00247 -0.1090 0.7034 0.0436
-0.500 0.5523 0.00911 0.00212 -0.1089 0.6767 0.0463
-0.250 0.5804 0.00906 0.00203 -0.1089 0.6651 0.0505
0.000 0.6083 0.00903 0.00204 -0.1089 0.6549 0.0653
0.250 0.6360 0.00912 0.00212 -0.1089 0.6451 0.0914
0.500 0.6640 0.00920 0.00220 -0.1089 0.6352 0.1038
0.750 0.6917 0.00930 0.00225 -0.1089 0.6261 0.1108
1.000 0.7194 0.00935 0.00229 -0.1089 0.6171 0.1179
1.250 0.7473 0.00940 0.00233 -0.1090 0.6086 0.1246
1.750 0.8028 0.00947 0.00242 -0.1092 0.5915 0.1405
2.000 0.8304 0.00950 0.00248 -0.1092 0.5827 0.1582
2.250 0.8523 0.00788 0.00266 -0.1083 0.5737 1.0000
2.500 0.8798 0.00801 0.00273 -0.1083 0.5633 1.0000
2.750 0.9070 0.00814 0.00280 -0.1083 0.5515 1.0000
3.000 0.9341 0.00829 0.00288 -0.1082 0.5389 1.0000
3.250 0.9610 0.00844 0.00297 -0.1081 0.5251 1.0000
3.500 0.9878 0.00860 0.00309 -0.1080 0.5101 1.0000
3.750 1.0144 0.00877 0.00321 -0.1079 0.4938 1.0000
4.000 1.0407 0.00897 0.00336 -0.1078 0.4755 1.0000
4.250 1.0665 0.00922 0.00353 -0.1075 0.4554 1.0000
4.500 1.0918 0.00951 0.00373 -0.1073 0.4328 1.0000
4.750 1.1163 0.00987 0.00396 -0.1069 0.4079 1.0000
5.000 1.1411 0.01021 0.00420 -0.1066 0.3852 1.0000
5.250 1.1657 0.01057 0.00448 -0.1062 0.3657 1.0000
5.500 1.1902 0.01092 0.00477 -0.1058 0.3480 1.0000
5.750 1.2146 0.01127 0.00506 -0.1055 0.3292 1.0000
6.000 1.2387 0.01165 0.00537 -0.1051 0.3100 1.0000
6.250 1.2621 0.01207 0.00572 -0.1046 0.2900 1.0000
6.500 1.2848 0.01256 0.00609 -0.1040 0.2601 1.0000
6.750 1.3000 0.01373 0.00678 -0.1024 0.1815 1.0000
7.000 1.3077 0.01558 0.00802 -0.0997 0.0897 1.0000
7.250 1.3244 0.01653 0.00881 -0.0982 0.0618 1.0000
7.500 1.3361 0.01786 0.00986 -0.0959 0.0228 1.0000
7.750 1.3539 0.01860 0.01064 -0.0945 0.0195 1.0000
8.000 1.3718 0.01928 0.01141 -0.0931 0.0180 1.0000
8.250 1.3881 0.02002 0.01224 -0.0914 0.0169 1.0000
8.500 1.4017 0.02087 0.01318 -0.0894 0.0160 1.0000
8.750 1.4104 0.02185 0.01426 -0.0865 0.0153 1.0000
9.000 1.4159 0.02308 0.01559 -0.0833 0.0147 1.0000
9.250 1.4173 0.02466 0.01729 -0.0799 0.0142 1.0000
9.500 1.4196 0.02629 0.01903 -0.0770 0.0139 1.0000
9.750 1.4266 0.02766 0.02049 -0.0748 0.0137 1.0000
10.000 1.4328 0.02917 0.02210 -0.0728 0.0134 1.0000
10.250 1.4378 0.03085 0.02387 -0.0709 0.0131 1.0000
10.500 1.4421 0.03266 0.02579 -0.0690 0.0127 1.0000
10.750 1.4453 0.03463 0.02785 -0.0673 0.0123 1.0000
11.000 1.4473 0.03679 0.03009 -0.0657 0.0120 1.0000
11.250 1.4487 0.03908 0.03247 -0.0641 0.0117 1.0000
11.500 1.4497 0.04147 0.03495 -0.0627 0.0115 1.0000
11.750 1.4504 0.04395 0.03751 -0.0614 0.0113 1.0000
12.000 1.4507 0.04651 0.04014 -0.0601 0.0111 1.0000
12.250 1.4515 0.04907 0.04277 -0.0588 0.0110 1.0000
12.500 1.4527 0.05159 0.04537 -0.0573 0.0108 1.0000
12.750 1.4560 0.05393 0.04775 -0.0556 0.0106 1.0000
13.000 1.4642 0.05596 0.04984 -0.0534 0.0105 1.0000
13.250 1.4783 0.05800 0.05196 -0.0512 0.0103 1.0000
13.500 1.4891 0.06052 0.05462 -0.0496 0.0103 1.0000
13.750 1.4833 0.06369 0.05797 -0.0490 0.0102 1.0000
14.000 1.4766 0.06704 0.06150 -0.0488 0.0102 1.0000
14.250 1.4705 0.07058 0.06523 -0.0487 0.0101 1.0000
14.500 1.4636 0.07438 0.06921 -0.0490 0.0100 1.0000
14.750 1.4568 0.07841 0.07342 -0.0495 0.0099 1.0000
15.000 1.4492 0.08272 0.07793 -0.0501 0.0098 1.0000
15.250 1.4407 0.08732 0.08270 -0.0511 0.0097 1.0000
15.500 1.4311 0.09219 0.08775 -0.0522 0.0097 1.0000
15.750 1.4205 0.09741 0.09315 -0.0536 0.0097 1.0000
16.000 1.4090 0.10293 0.09885 -0.0554 0.0097 1.0000
16.250 1.3964 0.10881 0.10490 -0.0574 0.0098 1.0000
16.500 1.3827 0.11502 0.11128 -0.0598 0.0099 1.0000
16.750 1.3682 0.12159 0.11803 -0.0625 0.0100 1.0000
17.000 1.3809 0.12287 0.11932 -0.0614 0.0106 1.0000
17.250 1.1174 0.11864 0.11537 -0.0421 0.0106 1.0000
17.500 1.0995 0.12396 0.12085 -0.0450 0.0107 1.0000
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