FX 66-S-196 V1 AIRFOIL (fx66196v-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 66-S-196 V1 AIRFOIL (fx66196v-il) Reynolds number: 1,000,000 Max Cl/Cd: 132.69 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx66196v-il-1000000-n5.txt Download as CSV file: xf-fx66196v-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 66-S-196 V1 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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7780 0.09188 0.08913 -0.0680 0.9484 0.0059
-18.000 -0.7816 0.08248 0.07950 -0.0783 0.9319 0.0059
-17.750 -0.7639 0.07444 0.07120 -0.0908 0.9114 0.0060
-17.500 -0.7549 0.06647 0.06287 -0.1023 0.8777 0.0060
-17.250 -0.7502 0.06189 0.05801 -0.1073 0.8416 0.0060
-17.000 -0.7532 0.05792 0.05387 -0.1099 0.8281 0.0061
-16.750 -0.7488 0.05509 0.05087 -0.1118 0.8081 0.0062
-16.500 -0.7516 0.05167 0.04729 -0.1136 0.7897 0.0062
-16.250 -0.7499 0.04893 0.04440 -0.1150 0.7753 0.0063
-16.000 -0.7466 0.04650 0.04184 -0.1160 0.7618 0.0063
-15.750 -0.7445 0.04409 0.03928 -0.1169 0.7461 0.0064
-15.500 -0.7433 0.04168 0.03673 -0.1176 0.7338 0.0064
-15.250 -0.7342 0.04012 0.03506 -0.1181 0.7220 0.0065
-15.000 -0.7334 0.03791 0.03274 -0.1184 0.7114 0.0065
-14.750 -0.7319 0.03586 0.03059 -0.1186 0.7011 0.0067
-14.500 -0.7290 0.03399 0.02862 -0.1186 0.6930 0.0068
-14.250 -0.7243 0.03233 0.02686 -0.1185 0.6836 0.0068
-13.750 -0.7100 0.02949 0.02387 -0.1180 0.6663 0.0071
-13.250 -0.6914 0.02710 0.02134 -0.1173 0.6517 0.0074
-13.000 -0.6831 0.02589 0.02005 -0.1167 0.6446 0.0075
-12.750 -0.6706 0.02497 0.01907 -0.1163 0.6389 0.0077
-12.500 -0.6618 0.02383 0.01786 -0.1157 0.6327 0.0078
-12.250 -0.6509 0.02286 0.01682 -0.1150 0.6273 0.0080
-12.000 -0.6404 0.02187 0.01577 -0.1142 0.6220 0.0081
-11.750 -0.6296 0.02094 0.01477 -0.1134 0.6163 0.0083
-11.500 -0.6187 0.02007 0.01383 -0.1125 0.6110 0.0084
-11.250 -0.6088 0.01917 0.01288 -0.1113 0.6060 0.0085
-11.000 -0.5985 0.01840 0.01203 -0.1101 0.6006 0.0086
-10.750 -0.5903 0.01768 0.01125 -0.1083 0.5961 0.0088
-10.500 -0.5861 0.01706 0.01057 -0.1056 0.5919 0.0089
-10.250 -0.5728 0.01648 0.00993 -0.1042 0.5874 0.0093
-10.000 -0.5561 0.01601 0.00941 -0.1031 0.5830 0.0096
-9.750 -0.5371 0.01559 0.00895 -0.1023 0.5795 0.0099
-9.500 -0.5167 0.01519 0.00851 -0.1017 0.5760 0.0102
-9.250 -0.4954 0.01483 0.00810 -0.1011 0.5723 0.0106
-9.000 -0.4735 0.01449 0.00770 -0.1006 0.5687 0.0110
-8.750 -0.4506 0.01418 0.00733 -0.1002 0.5655 0.0113
-8.500 -0.4274 0.01383 0.00695 -0.0999 0.5627 0.0119
-8.250 -0.4037 0.01349 0.00659 -0.0997 0.5596 0.0126
-8.000 -0.3794 0.01320 0.00627 -0.0995 0.5564 0.0133
-7.750 -0.3545 0.01295 0.00597 -0.0994 0.5533 0.0141
-7.500 -0.3292 0.01272 0.00569 -0.0993 0.5503 0.0148
-7.250 -0.3038 0.01242 0.00539 -0.0993 0.5480 0.0160
-7.000 -0.2779 0.01217 0.00512 -0.0993 0.5453 0.0173
-6.750 -0.2515 0.01197 0.00488 -0.0993 0.5426 0.0186
-6.500 -0.2253 0.01173 0.00463 -0.0994 0.5399 0.0206
-6.250 -0.1988 0.01154 0.00441 -0.0995 0.5372 0.0230
-6.000 -0.1722 0.01133 0.00419 -0.0996 0.5349 0.0263
-5.750 -0.1450 0.01113 0.00399 -0.0998 0.5330 0.0302
-5.500 -0.1179 0.01093 0.00380 -0.1000 0.5309 0.0357
-5.250 -0.0908 0.01072 0.00360 -0.1002 0.5288 0.0444
-5.000 -0.0637 0.01050 0.00341 -0.1004 0.5266 0.0567
-4.750 -0.0367 0.01026 0.00323 -0.1006 0.5244 0.0739
-4.500 -0.0099 0.01000 0.00304 -0.1008 0.5222 0.0999
-4.000 0.0433 0.00930 0.00263 -0.1013 0.5187 0.1886
-3.750 0.0692 0.00877 0.00238 -0.1015 0.5174 0.2673
-3.500 0.0947 0.00820 0.00211 -0.1017 0.5159 0.3580
-3.250 0.1216 0.00791 0.00205 -0.1019 0.5144 0.4334
-3.000 0.1503 0.00789 0.00204 -0.1023 0.5129 0.4521
-2.750 0.1790 0.00789 0.00204 -0.1026 0.5114 0.4659
-2.500 0.2079 0.00792 0.00205 -0.1029 0.5099 0.4763
-2.250 0.2366 0.00795 0.00207 -0.1032 0.5085 0.4841
-2.000 0.2654 0.00801 0.00207 -0.1036 0.5070 0.4901
-1.750 0.2939 0.00803 0.00208 -0.1039 0.5055 0.4943
-1.500 0.3226 0.00805 0.00208 -0.1042 0.5043 0.4972
-1.250 0.3516 0.00806 0.00208 -0.1046 0.5035 0.4996
-1.000 0.3805 0.00808 0.00209 -0.1049 0.5025 0.5017
-0.750 0.4094 0.00810 0.00209 -0.1053 0.5015 0.5035
-0.500 0.4383 0.00813 0.00210 -0.1057 0.5005 0.5049
-0.250 0.4671 0.00816 0.00211 -0.1060 0.4994 0.5059
0.000 0.4957 0.00818 0.00212 -0.1064 0.4982 0.5071
0.250 0.5242 0.00820 0.00214 -0.1067 0.4972 0.5087
0.500 0.5527 0.00823 0.00217 -0.1070 0.4961 0.5102
0.750 0.5811 0.00826 0.00221 -0.1073 0.4950 0.5117
1.000 0.6094 0.00831 0.00224 -0.1076 0.4940 0.5132
1.250 0.6376 0.00835 0.00229 -0.1079 0.4929 0.5148
1.500 0.6657 0.00841 0.00234 -0.1082 0.4919 0.5164
1.750 0.6937 0.00847 0.00240 -0.1084 0.4908 0.5181
2.000 0.7216 0.00854 0.00247 -0.1087 0.4897 0.5197
2.250 0.7499 0.00859 0.00253 -0.1090 0.4890 0.5213
2.750 0.8064 0.00867 0.00266 -0.1096 0.4877 0.5248
3.000 0.8344 0.00872 0.00273 -0.1099 0.4869 0.5270
3.250 0.8625 0.00876 0.00281 -0.1101 0.4860 0.5295
3.500 0.8904 0.00881 0.00289 -0.1104 0.4851 0.5320
3.750 0.9183 0.00887 0.00298 -0.1107 0.4843 0.5344
4.000 0.9461 0.00893 0.00307 -0.1109 0.4835 0.5367
4.500 1.0011 0.00905 0.00326 -0.1113 0.4814 0.5416
4.750 1.0284 0.00912 0.00336 -0.1115 0.4804 0.5446
5.000 1.0556 0.00919 0.00347 -0.1116 0.4794 0.5476
5.250 1.0826 0.00927 0.00358 -0.1118 0.4784 0.5507
5.500 1.1093 0.00937 0.00370 -0.1118 0.4771 0.5535
5.750 1.1357 0.00946 0.00383 -0.1119 0.4756 0.5567
6.000 1.1621 0.00956 0.00397 -0.1119 0.4741 0.5604
6.250 1.1889 0.00962 0.00410 -0.1120 0.4730 0.5643
6.500 1.2156 0.00969 0.00423 -0.1121 0.4718 0.5680
6.750 1.2420 0.00975 0.00436 -0.1121 0.4702 0.5717
7.000 1.2681 0.00982 0.00449 -0.1121 0.4684 0.5761
7.250 1.2935 0.00989 0.00462 -0.1119 0.4659 0.5808
7.500 1.3155 0.01002 0.00475 -0.1111 0.4599 0.5853
7.750 1.3375 0.01008 0.00484 -0.1103 0.4478 0.5906
8.000 1.3565 0.01026 0.00501 -0.1090 0.4322 0.5963
8.250 1.3607 0.01072 0.00532 -0.1049 0.3914 0.6017
8.500 1.3380 0.01208 0.00637 -0.0963 0.3361 0.6069
8.750 1.3243 0.01336 0.00749 -0.0899 0.3010 0.6130
9.000 1.3037 0.01510 0.00904 -0.0831 0.2605 0.6185
9.250 1.2925 0.01674 0.01059 -0.0783 0.2336 0.6251
9.500 1.2815 0.01863 0.01239 -0.0742 0.2089 0.6321
9.750 1.2717 0.02069 0.01440 -0.0706 0.1866 0.6392
10.000 1.2628 0.02292 0.01658 -0.0676 0.1668 0.6474
10.250 1.2529 0.02541 0.01904 -0.0648 0.1467 0.6559
10.500 1.2422 0.02812 0.02170 -0.0623 0.1278 0.6653
10.750 1.2313 0.03100 0.02455 -0.0600 0.1081 0.6760
11.000 1.2219 0.03388 0.02741 -0.0581 0.0909 0.6871
11.250 1.2180 0.03646 0.02999 -0.0567 0.0779 0.7003
11.500 1.2131 0.03919 0.03272 -0.0554 0.0638 0.7160
11.750 1.2089 0.04198 0.03552 -0.0543 0.0495 0.7344
12.000 1.2089 0.04447 0.03805 -0.0536 0.0395 0.7575
12.250 1.2124 0.04681 0.04048 -0.0532 0.0323 0.7934
12.500 1.2365 0.04976 0.04373 -0.0579 0.0235 0.9019
13.000 1.2987 0.05628 0.05034 -0.0700 0.0128 1.0000
13.250 1.3038 0.05854 0.05262 -0.0696 0.0114 1.0000
13.500 1.3110 0.06059 0.05470 -0.0693 0.0103 1.0000
13.750 1.3173 0.06275 0.05690 -0.0691 0.0098 1.0000
14.000 1.3233 0.06493 0.05910 -0.0688 0.0090 1.0000
14.250 1.3295 0.06708 0.06129 -0.0685 0.0083 1.0000
14.500 1.3357 0.06927 0.06352 -0.0683 0.0079 1.0000
14.750 1.3424 0.07139 0.06567 -0.0681 0.0075 1.0000
15.000 1.3482 0.07361 0.06793 -0.0678 0.0070 1.0000
15.250 1.3522 0.07605 0.07041 -0.0676 0.0065 1.0000
15.500 1.3582 0.07824 0.07263 -0.0674 0.0063 1.0000
15.750 1.3646 0.08039 0.07483 -0.0673 0.0061 1.0000
16.000 1.3695 0.08277 0.07726 -0.0672 0.0058 1.0000
16.250 1.3750 0.08505 0.07958 -0.0671 0.0056 1.0000
16.500 1.3802 0.08737 0.08193 -0.0670 0.0053 1.0000
16.750 1.3836 0.08992 0.08454 -0.0669 0.0051 1.0000
17.000 1.3870 0.09244 0.08709 -0.0669 0.0048 1.0000
17.250 1.3908 0.09490 0.08961 -0.0668 0.0047 1.0000
17.500 1.3933 0.09758 0.09233 -0.0668 0.0046 1.0000
17.750 1.3970 0.10010 0.09490 -0.0669 0.0045 1.0000
18.000 1.4019 0.10248 0.09734 -0.0670 0.0043 1.0000
18.250 1.4041 0.10522 0.10013 -0.0671 0.0042 1.0000
18.500 1.4067 0.10789 0.10286 -0.0673 0.0041 1.0000
18.750 1.4098 0.11047 0.10550 -0.0675 0.0039 1.0000
19.000 1.4117 0.11324 0.10832 -0.0678 0.0038 1.0000
19.250 1.4132 0.11609 0.11122 -0.0681 0.0037 1.0000
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