FX S 02/1-158 AIRFOIL (fxs21158-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX S 02/1-158 AIRFOIL (fxs21158-il) Reynolds number: 1,000,000 Max Cl/Cd: 105.14 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxs21158-il-1000000.txt Download as CSV file: xf-fxs21158-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX S 02/1-158 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
------ -------- --------- --------- -------- -------- --------
-14.250 -0.7557 0.07002 0.06797 -0.0460 1.0000 0.0024
-14.000 -0.7858 0.06066 0.05844 -0.0524 1.0000 0.0024
-13.750 -0.8124 0.05320 0.05080 -0.0574 1.0000 0.0024
-13.500 -0.8237 0.04843 0.04591 -0.0604 1.0000 0.0024
-13.250 -0.8429 0.04287 0.04015 -0.0637 1.0000 0.0024
-13.000 -0.8480 0.03928 0.03645 -0.0657 1.0000 0.0024
-12.750 -0.8539 0.03569 0.03272 -0.0676 1.0000 0.0024
-12.500 -0.8538 0.03296 0.02988 -0.0689 1.0000 0.0024
-12.250 -0.8622 0.02967 0.02643 -0.0700 1.0000 0.0024
-12.000 -0.8635 0.02729 0.02394 -0.0708 1.0000 0.0024
-11.750 -0.8321 0.02454 0.02095 -0.0768 0.9616 0.0024
-11.500 -0.7353 0.02138 0.01726 -0.0953 0.8834 0.0025
-11.250 -0.7244 0.02062 0.01611 -0.0938 0.8047 0.0025
-11.000 -0.7120 0.01976 0.01496 -0.0924 0.7605 0.0026
-10.750 -0.6960 0.01900 0.01397 -0.0913 0.7264 0.0026
-10.500 -0.6771 0.01834 0.01313 -0.0906 0.6994 0.0026
-10.250 -0.6577 0.01763 0.01224 -0.0900 0.6769 0.0027
-10.000 -0.6367 0.01697 0.01142 -0.0895 0.6579 0.0027
-9.750 -0.6146 0.01637 0.01067 -0.0890 0.6392 0.0028
-9.500 -0.5929 0.01566 0.00977 -0.0886 0.6214 0.0032
-9.250 -0.5699 0.01507 0.00904 -0.0882 0.6068 0.0036
-9.000 -0.5460 0.01453 0.00838 -0.0880 0.5933 0.0039
-8.750 -0.5221 0.01392 0.00768 -0.0878 0.5806 0.0051
-8.500 -0.4964 0.01362 0.00747 -0.0877 0.5680 0.0093
-8.250 -0.4685 0.01369 0.00754 -0.0878 0.5572 0.0119
-8.000 -0.4405 0.01380 0.00761 -0.0878 0.5478 0.0137
-7.750 -0.4116 0.01402 0.00783 -0.0879 0.5400 0.0147
-7.500 -0.3833 0.01418 0.00795 -0.0879 0.5334 0.0151
-7.250 -0.3540 0.01445 0.00820 -0.0881 0.5277 0.0154
-7.000 -0.3314 0.01335 0.00698 -0.0879 0.5227 0.0169
-6.750 -0.3043 0.01316 0.00677 -0.0880 0.5181 0.0180
-6.500 -0.2764 0.01305 0.00666 -0.0882 0.5136 0.0190
-6.250 -0.2490 0.01289 0.00645 -0.0883 0.5092 0.0199
-6.000 -0.2215 0.01276 0.00628 -0.0883 0.5052 0.0209
-5.750 -0.1934 0.01266 0.00615 -0.0884 0.5017 0.0218
-5.500 -0.1655 0.01255 0.00599 -0.0885 0.4977 0.0223
-5.250 -0.1379 0.01241 0.00579 -0.0886 0.4931 0.0227
-5.000 -0.1122 0.01157 0.00484 -0.0886 0.4891 0.0237
-4.750 -0.0849 0.01114 0.00434 -0.0888 0.4843 0.0251
-4.500 -0.0573 0.01090 0.00403 -0.0889 0.4798 0.0261
-4.250 -0.0293 0.01067 0.00372 -0.0890 0.4762 0.0264
-4.000 -0.0009 0.01043 0.00343 -0.0892 0.4734 0.0267
-3.750 0.0275 0.01022 0.00318 -0.0893 0.4705 0.0270
-3.500 0.0558 0.01006 0.00295 -0.0895 0.4673 0.0274
-3.250 0.0841 0.00994 0.00277 -0.0896 0.4644 0.0282
-3.000 0.1126 0.00982 0.00260 -0.0897 0.4619 0.0290
-2.750 0.1414 0.00969 0.00244 -0.0899 0.4600 0.0300
-2.500 0.1703 0.00958 0.00230 -0.0901 0.4578 0.0317
-2.250 0.1989 0.00934 0.00212 -0.0903 0.4552 0.0676
-2.000 0.2274 0.00912 0.00199 -0.0906 0.4526 0.1076
-1.750 0.2552 0.00875 0.00182 -0.0909 0.4487 0.1931
-1.500 0.2823 0.00786 0.00155 -0.0915 0.4459 0.3860
-1.250 0.3111 0.00779 0.00157 -0.0917 0.4425 0.4269
-1.000 0.3400 0.00781 0.00157 -0.0918 0.4394 0.4398
-0.750 0.3687 0.00784 0.00159 -0.0920 0.4369 0.4503
-0.500 0.3974 0.00789 0.00161 -0.0921 0.4344 0.4563
-0.250 0.4262 0.00791 0.00163 -0.0923 0.4326 0.4611
0.000 0.4552 0.00794 0.00165 -0.0925 0.4305 0.4655
0.250 0.4839 0.00798 0.00168 -0.0926 0.4281 0.4720
0.500 0.5126 0.00804 0.00174 -0.0928 0.4255 0.4798
0.750 0.5413 0.00810 0.00176 -0.0929 0.4232 0.4824
1.000 0.5696 0.00815 0.00180 -0.0930 0.4203 0.4852
1.250 0.5984 0.00817 0.00183 -0.0932 0.4168 0.4884
1.500 0.6269 0.00821 0.00186 -0.0934 0.4114 0.4912
1.750 0.6550 0.00830 0.00191 -0.0935 0.4064 0.4938
2.000 0.6836 0.00835 0.00195 -0.0936 0.4038 0.4959
2.250 0.7123 0.00839 0.00199 -0.0938 0.4007 0.4978
2.500 0.7406 0.00842 0.00204 -0.0940 0.3970 0.5004
2.750 0.7688 0.00848 0.00211 -0.0941 0.3929 0.5031
3.000 0.7970 0.00854 0.00217 -0.0942 0.3892 0.5056
3.250 0.8254 0.00859 0.00224 -0.0943 0.3843 0.5083
3.500 0.8535 0.00867 0.00230 -0.0945 0.3783 0.5106
3.750 0.8815 0.00875 0.00238 -0.0946 0.3713 0.5127
4.250 0.9364 0.00896 0.00258 -0.0946 0.3548 0.5194
4.500 0.9631 0.00916 0.00274 -0.0946 0.3420 0.5238
4.750 0.9826 0.01006 0.00325 -0.0935 0.2733 0.5271
5.000 0.9954 0.01155 0.00424 -0.0916 0.1717 0.5308
5.250 1.0169 0.01218 0.00471 -0.0908 0.1337 0.5337
5.500 1.0373 0.01288 0.00526 -0.0899 0.0928 0.5368
5.750 1.0614 0.01324 0.00558 -0.0894 0.0841 0.5401
6.000 1.0869 0.01345 0.00582 -0.0892 0.0784 0.5434
6.250 1.1074 0.01405 0.00631 -0.0883 0.0515 0.5470
6.500 1.1320 0.01430 0.00660 -0.0879 0.0468 0.5516
6.750 1.1513 0.01495 0.00718 -0.0868 0.0270 0.5554
7.000 1.1744 0.01526 0.00753 -0.0863 0.0230 0.5603
7.250 1.1970 0.01558 0.00789 -0.0856 0.0190 0.5655
7.500 1.2125 0.01637 0.00861 -0.0840 0.0041 0.5699
7.750 1.2328 0.01678 0.00907 -0.0830 0.0035 0.5748
8.000 1.2523 0.01721 0.00955 -0.0819 0.0031 0.5806
8.250 1.2706 0.01767 0.01009 -0.0806 0.0029 0.5869
8.500 1.2871 0.01816 0.01067 -0.0791 0.0028 0.5944
8.750 1.2993 0.01870 0.01128 -0.0768 0.0027 0.6029
9.000 1.3069 0.01933 0.01200 -0.0739 0.0025 0.6137
9.250 1.3132 0.02006 0.01283 -0.0709 0.0024 0.6270
9.500 1.3150 0.02105 0.01394 -0.0677 0.0023 0.6435
9.750 1.3182 0.02210 0.01513 -0.0652 0.0023 0.6692
10.000 1.3186 0.02345 0.01668 -0.0628 0.0023 0.7147
10.250 1.3203 0.02506 0.01891 -0.0618 0.0022 1.0000
10.500 1.3219 0.02716 0.02109 -0.0609 0.0022 1.0000
10.750 1.3214 0.02968 0.02369 -0.0602 0.0021 1.0000
11.000 1.3210 0.03234 0.02644 -0.0598 0.0021 1.0000
11.250 1.3147 0.03567 0.02988 -0.0594 0.0021 1.0000
11.500 1.3170 0.03817 0.03243 -0.0591 0.0021 1.0000
11.750 1.3113 0.04151 0.03586 -0.0588 0.0021 1.0000
12.000 1.3071 0.04474 0.03917 -0.0587 0.0021 1.0000
12.250 1.3010 0.04818 0.04269 -0.0585 0.0021 1.0000
12.500 1.2984 0.05128 0.04586 -0.0584 0.0021 1.0000
12.750 1.2946 0.05457 0.04923 -0.0584 0.0021 1.0000
13.000 1.2924 0.05781 0.05254 -0.0586 0.0021 1.0000
13.250 1.2895 0.06125 0.05605 -0.0588 0.0021 1.0000
13.500 1.2905 0.06424 0.05910 -0.0591 0.0021 1.0000
13.750 1.2875 0.06783 0.06277 -0.0594 0.0021 1.0000
14.000 1.2876 0.07107 0.06608 -0.0598 0.0021 1.0000
14.250 1.2865 0.07450 0.06959 -0.0603 0.0022 1.0000
14.500 1.2876 0.07771 0.07287 -0.0608 0.0022 1.0000
14.750 1.2855 0.08139 0.07664 -0.0613 0.0023 1.0000
15.000 1.2876 0.08452 0.07985 -0.0619 0.0023 1.0000
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