FX 62-K-153/20 AIRFOIL (fx62k153-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 62-K-153/20 AIRFOIL (fx62k153-il) Reynolds number: 100,000 Max Cl/Cd: 44.11 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx62k153-il-100000-n5.txt Download as CSV file: xf-fx62k153-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 62-K-153/20 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.000 -0.1125 0.10682 0.10187 -0.1001 0.9404 0.0276
-11.750 -0.2410 0.11771 0.11264 -0.0884 0.9618 0.0283
-11.500 -0.2290 0.11428 0.10919 -0.0896 0.9584 0.0273
-11.250 -0.2209 0.11001 0.10490 -0.0923 0.9543 0.0264
-11.000 -0.2136 0.10516 0.10005 -0.0958 0.9510 0.0256
-10.750 -0.2072 0.09981 0.09471 -0.1000 0.9482 0.0248
-10.500 -0.2053 0.09439 0.08930 -0.1037 0.9435 0.0241
-10.000 -0.2256 0.07281 0.06767 -0.1215 0.9341 0.0214
-9.750 -0.2349 0.06749 0.06228 -0.1257 0.9273 0.0213
-9.500 -0.2444 0.06228 0.05693 -0.1301 0.9213 0.0211
-9.250 -0.2579 0.05841 0.05292 -0.1320 0.9137 0.0210
-9.000 -0.2704 0.05496 0.04928 -0.1331 0.9069 0.0210
-8.750 -0.2798 0.05177 0.04584 -0.1337 0.9003 0.0210
-8.500 -0.2848 0.04856 0.04232 -0.1335 0.8940 0.0210
-8.250 -0.2795 0.04452 0.03770 -0.1348 0.8903 0.0215
-8.000 -0.2820 0.04290 0.03598 -0.1322 0.8839 0.0221
-7.750 -0.2672 0.04166 0.03467 -0.1323 0.8802 0.0235
-7.500 -0.2479 0.03940 0.03205 -0.1332 0.8774 0.0251
-7.250 -0.2247 0.03639 0.02851 -0.1343 0.8754 0.0263
-7.000 -0.2224 0.03508 0.02691 -0.1308 0.8691 0.0270
-6.750 -0.2007 0.03321 0.02457 -0.1305 0.8659 0.0290
-6.500 -0.1751 0.03169 0.02297 -0.1313 0.8637 0.0314
-6.250 -0.1466 0.03016 0.02121 -0.1318 0.8621 0.0332
-6.000 -0.1172 0.02886 0.01967 -0.1322 0.8607 0.0357
-5.750 -0.1128 0.02875 0.01943 -0.1283 0.8542 0.0377
-5.500 -0.0909 0.02768 0.01838 -0.1277 0.8513 0.0404
-5.250 -0.0647 0.02683 0.01751 -0.1277 0.8492 0.0433
-5.000 -0.0359 0.02608 0.01666 -0.1282 0.8475 0.0478
-4.750 -0.0050 0.02525 0.01581 -0.1294 0.8461 0.0547
-4.500 0.0009 0.02533 0.01586 -0.1262 0.8393 0.0596
-4.250 0.0282 0.02478 0.01529 -0.1270 0.8366 0.0725
-4.000 0.0607 0.02403 0.01466 -0.1288 0.8345 0.1054
-3.750 0.1033 0.02174 0.01426 -0.1347 0.8335 0.4669
-3.500 0.1228 0.02246 0.01527 -0.1312 0.8316 0.5894
-3.250 0.1321 0.02345 0.01618 -0.1280 0.8249 0.6271
-2.750 0.1653 0.02538 0.01797 -0.1206 0.8186 0.6841
-2.250 0.1875 0.02673 0.01917 -0.1134 0.8086 0.7105
-2.000 0.2194 0.02672 0.01898 -0.1148 0.8061 0.7171
-1.750 0.2516 0.02666 0.01876 -0.1158 0.8041 0.7219
-1.500 0.2830 0.02658 0.01856 -0.1165 0.8025 0.7259
-1.250 0.2920 0.02719 0.01911 -0.1144 0.7947 0.7316
-1.000 0.3224 0.02720 0.01902 -0.1154 0.7916 0.7360
-0.750 0.3527 0.02715 0.01887 -0.1160 0.7895 0.7392
-0.250 0.3999 0.02768 0.01927 -0.1163 0.7797 0.7484
0.000 0.4274 0.02770 0.01923 -0.1165 0.7765 0.7514
0.250 0.4595 0.02758 0.01907 -0.1173 0.7743 0.7544
0.500 0.4955 0.02743 0.01885 -0.1190 0.7728 0.7578
1.000 0.5366 0.02816 0.01957 -0.1183 0.7607 0.7651
1.250 0.5698 0.02797 0.01936 -0.1192 0.7588 0.7678
1.750 0.6107 0.02868 0.02010 -0.1182 0.7465 0.7744
2.000 0.6495 0.02844 0.01984 -0.1205 0.7445 0.7779
2.250 0.6849 0.02809 0.01952 -0.1217 0.7429 0.7803
2.500 0.6885 0.02905 0.02055 -0.1186 0.7318 0.7833
2.750 0.7232 0.02873 0.02025 -0.1198 0.7298 0.7861
3.250 0.7700 0.02955 0.02118 -0.1200 0.7171 0.7929
3.500 0.8026 0.02918 0.02088 -0.1206 0.7150 0.7950
4.000 0.8434 0.02997 0.02186 -0.1194 0.7018 0.8009
4.250 0.8797 0.02955 0.02151 -0.1208 0.7001 0.8039
4.500 0.8917 0.03068 0.02273 -0.1197 0.6887 0.8071
4.750 0.9266 0.02992 0.02209 -0.1203 0.6863 0.8094
5.000 0.9384 0.03057 0.02285 -0.1184 0.6747 0.8123
5.250 0.9769 0.02952 0.02190 -0.1194 0.6717 0.8152
5.500 0.9917 0.03012 0.02261 -0.1181 0.6598 0.8184
6.000 1.0448 0.02978 0.02254 -0.1178 0.6445 0.8240
6.500 1.0961 0.02943 0.02248 -0.1171 0.6288 0.8301
6.750 1.1160 0.02964 0.02283 -0.1162 0.6158 0.8333
7.000 1.1429 0.02929 0.02258 -0.1159 0.6010 0.8364
7.250 1.1711 0.02855 0.02193 -0.1151 0.5842 0.8391
7.500 1.1876 0.02883 0.02233 -0.1135 0.5634 0.8424
7.750 1.2157 0.02834 0.02188 -0.1130 0.5411 0.8459
8.000 1.2377 0.02843 0.02198 -0.1121 0.5135 0.8494
8.250 1.2588 0.02854 0.02205 -0.1109 0.4823 0.8524
8.500 1.2738 0.02904 0.02248 -0.1090 0.4489 0.8556
8.750 1.2845 0.02991 0.02327 -0.1069 0.4117 0.8593
9.000 1.2918 0.03114 0.02435 -0.1046 0.3728 0.8632
9.250 1.2939 0.03272 0.02576 -0.1019 0.3294 0.8669
9.500 1.2919 0.03458 0.02740 -0.0988 0.2898 0.8705
9.750 1.2909 0.03658 0.02922 -0.0962 0.2516 0.8743
10.000 1.2897 0.03873 0.03119 -0.0938 0.2168 0.8781
10.250 1.2894 0.04079 0.03313 -0.0915 0.1844 0.8822
10.500 1.2887 0.04290 0.03512 -0.0893 0.1578 0.8867
10.750 1.2903 0.04497 0.03716 -0.0874 0.1374 0.8916
11.000 1.2922 0.04700 0.03918 -0.0855 0.1214 0.8967
11.250 1.2942 0.04902 0.04122 -0.0837 0.1083 0.9024
11.750 1.2985 0.05317 0.04547 -0.0804 0.0887 0.9161
12.000 1.3004 0.05523 0.04763 -0.0788 0.0812 0.9266
12.250 1.3005 0.05727 0.04975 -0.0769 0.0753 0.9455
12.500 1.3010 0.05938 0.05199 -0.0755 0.0694 0.9999
12.750 1.3045 0.06207 0.05471 -0.0749 0.0642 0.9999
13.000 1.3104 0.06453 0.05732 -0.0745 0.0590 0.9999
13.250 1.3127 0.06737 0.06024 -0.0740 0.0554 0.9999
13.500 1.3177 0.06995 0.06296 -0.0736 0.0511 0.9999
13.750 1.3217 0.07275 0.06589 -0.0735 0.0463 0.9999
14.000 1.3225 0.07593 0.06912 -0.0736 0.0420 0.9999
14.250 1.3266 0.07885 0.07222 -0.0739 0.0370 0.9999
14.500 1.3242 0.08253 0.07591 -0.0743 0.0335 0.9999
14.750 1.3281 0.08554 0.07916 -0.0746 0.0293 0.9999
15.000 1.3265 0.08925 0.08299 -0.0750 0.0268 0.9999
15.250 1.3220 0.09336 0.08718 -0.0755 0.0249 0.9999
15.500 1.3207 0.09712 0.09116 -0.0759 0.0226 0.9999
15.750 1.3170 0.10131 0.09550 -0.0768 0.0207 0.9999
16.000 1.3108 0.10597 0.10025 -0.0781 0.0193 0.9999
16.250 1.3055 0.11049 0.10492 -0.0792 0.0180 0.9999
16.500 1.3010 0.11511 0.10977 -0.0807 0.0163 0.9999
16.750 1.2962 0.11983 0.11471 -0.0825 0.0155 0.9999
17.000 1.2907 0.12484 0.11985 -0.0847 0.0148 0.9999
17.250 1.2840 0.13021 0.12534 -0.0874 0.0141 0.9999
17.500 1.2772 0.13557 0.13082 -0.0902 0.0137 0.9999
17.750 1.2704 0.14119 0.13664 -0.0932 0.0132 0.9999
18.000 1.2623 0.14737 0.14306 -0.0967 0.0128 0.9999
18.250 1.2538 0.15385 0.14975 -0.1006 0.0125 0.9999
18.500 1.2435 0.16109 0.15721 -0.1053 0.0122 0.9999
18.750 1.2327 0.16879 0.16511 -0.1104 0.0122 0.9999
19.000 1.2200 0.17748 0.17399 -0.1165 0.0122 0.9999
19.250 1.2049 0.18755 0.18424 -0.1235 0.0123 0.9999
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