WORTMANN FX 73-170 A (fx73170a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 A (fx73170a-il) Reynolds number: 1,000,000 Max Cl/Cd: 144.05 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73170a-il-1000000-n5.txt Download as CSV file: xf-fx73170a-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 73-170 A
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
------ -------- --------- --------- -------- -------- --------
-11.250 -0.0157 0.09071 0.08740 -0.1240 0.6837 0.0055
-11.000 -0.0075 0.08778 0.08446 -0.1261 0.6819 0.0061
-10.500 -0.3599 0.02357 0.01897 -0.1461 0.6797 0.0047
-10.250 -0.3522 0.02222 0.01744 -0.1439 0.6775 0.0046
-10.000 -0.3501 0.02022 0.01517 -0.1410 0.6754 0.0049
-9.750 -0.3376 0.01906 0.01381 -0.1392 0.6733 0.0049
-9.500 -0.3133 0.01900 0.01372 -0.1389 0.6716 0.0046
-9.250 -0.3023 0.01747 0.01198 -0.1369 0.6698 0.0049
-9.000 -0.2842 0.01663 0.01100 -0.1357 0.6679 0.0050
-8.750 -0.2617 0.01629 0.01061 -0.1351 0.6659 0.0052
-8.500 -0.2416 0.01563 0.00984 -0.1342 0.6638 0.0052
-8.250 -0.2191 0.01525 0.00940 -0.1336 0.6617 0.0054
-8.000 -0.1991 0.01457 0.00858 -0.1326 0.6595 0.0054
-7.750 -0.1765 0.01417 0.00810 -0.1319 0.6576 0.0056
-7.500 -0.1534 0.01373 0.00759 -0.1314 0.6562 0.0058
-7.250 -0.1302 0.01330 0.00710 -0.1309 0.6546 0.0059
-7.000 -0.1065 0.01294 0.00669 -0.1304 0.6529 0.0062
-6.750 -0.0831 0.01255 0.00623 -0.1298 0.6512 0.0062
-6.500 -0.0588 0.01227 0.00589 -0.1294 0.6494 0.0066
-6.250 -0.0347 0.01198 0.00554 -0.1290 0.6477 0.0067
-6.000 -0.0113 0.01163 0.00513 -0.1284 0.6459 0.0067
-5.750 0.0120 0.01130 0.00475 -0.1278 0.6439 0.0071
-5.500 0.0363 0.01103 0.00445 -0.1274 0.6423 0.0073
-5.250 0.0616 0.01081 0.00421 -0.1272 0.6410 0.0078
-5.000 0.0872 0.01063 0.00402 -0.1270 0.6394 0.0083
-4.750 0.1123 0.01041 0.00377 -0.1267 0.6379 0.0084
-4.500 0.1378 0.01023 0.00356 -0.1264 0.6364 0.0090
-4.250 0.1628 0.01002 0.00333 -0.1261 0.6347 0.0099
-4.000 0.1883 0.00987 0.00317 -0.1259 0.6332 0.0106
-3.750 0.2140 0.00974 0.00302 -0.1257 0.6317 0.0119
-3.500 0.2392 0.00961 0.00285 -0.1254 0.6300 0.0128
-3.250 0.2646 0.00949 0.00273 -0.1251 0.6284 0.0148
-3.000 0.2906 0.00936 0.00261 -0.1250 0.6270 0.0176
-2.750 0.3168 0.00925 0.00250 -0.1249 0.6257 0.0207
-2.500 0.3428 0.00912 0.00241 -0.1248 0.6243 0.0269
-2.250 0.3687 0.00901 0.00233 -0.1246 0.6228 0.0353
-2.000 0.3946 0.00891 0.00225 -0.1245 0.6214 0.0450
-1.750 0.4196 0.00876 0.00218 -0.1242 0.6200 0.0698
-1.500 0.4439 0.00857 0.00212 -0.1238 0.6185 0.1125
-1.250 0.4660 0.00828 0.00206 -0.1230 0.6171 0.1965
-1.000 0.4864 0.00794 0.00200 -0.1219 0.6156 0.3011
-0.750 0.5062 0.00761 0.00196 -0.1207 0.6141 0.4076
-0.500 0.5239 0.00722 0.00193 -0.1190 0.6126 0.5343
-0.250 0.5388 0.00682 0.00196 -0.1165 0.6114 0.6736
0.000 0.5603 0.00675 0.00206 -0.1153 0.6100 0.7388
0.250 0.5854 0.00678 0.00213 -0.1148 0.6087 0.7610
0.500 0.6109 0.00683 0.00218 -0.1145 0.6073 0.7752
0.750 0.6366 0.00689 0.00222 -0.1142 0.6059 0.7854
1.000 0.6623 0.00694 0.00228 -0.1140 0.6044 0.7927
1.250 0.6881 0.00699 0.00231 -0.1138 0.6029 0.7975
1.500 0.7141 0.00705 0.00234 -0.1137 0.6014 0.8004
1.750 0.7404 0.00711 0.00238 -0.1136 0.5999 0.8027
2.000 0.7667 0.00717 0.00243 -0.1136 0.5984 0.8051
2.250 0.7934 0.00721 0.00248 -0.1136 0.5974 0.8073
2.500 0.8199 0.00726 0.00254 -0.1137 0.5962 0.8097
2.750 0.8462 0.00731 0.00260 -0.1137 0.5950 0.8121
3.000 0.8723 0.00736 0.00266 -0.1136 0.5935 0.8145
3.500 0.9242 0.00747 0.00279 -0.1135 0.5903 0.8192
3.750 0.9501 0.00753 0.00287 -0.1134 0.5888 0.8215
4.000 0.9757 0.00760 0.00295 -0.1133 0.5874 0.8238
4.250 1.0012 0.00769 0.00304 -0.1132 0.5859 0.8261
4.500 1.0264 0.00779 0.00313 -0.1131 0.5839 0.8283
4.750 1.0519 0.00785 0.00323 -0.1130 0.5826 0.8303
5.000 1.0763 0.00791 0.00332 -0.1126 0.5807 0.8322
5.250 1.1006 0.00796 0.00342 -0.1123 0.5778 0.8342
5.500 1.1242 0.00804 0.00351 -0.1118 0.5744 0.8362
5.750 1.1482 0.00815 0.00364 -0.1115 0.5714 0.8382
6.000 1.1724 0.00827 0.00378 -0.1112 0.5680 0.8402
6.250 1.1974 0.00836 0.00393 -0.1111 0.5633 0.8424
6.500 1.2215 0.00850 0.00409 -0.1109 0.5588 0.8447
6.750 1.2444 0.00869 0.00427 -0.1105 0.5540 0.8469
7.000 1.2705 0.00882 0.00446 -0.1107 0.5488 0.8488
7.250 1.2961 0.00901 0.00469 -0.1110 0.5430 0.8509
7.500 1.3207 0.00924 0.00495 -0.1111 0.5343 0.8532
7.750 1.3406 0.00969 0.00537 -0.1106 0.5162 0.8560
8.000 1.3563 0.01043 0.00604 -0.1097 0.4925 0.8596
8.500 1.3503 0.01494 0.01013 -0.1051 0.3941 0.8692
8.750 1.3371 0.01802 0.01299 -0.1019 0.3463 0.8753
9.000 1.3270 0.02075 0.01556 -0.0989 0.3065 0.8815
9.250 1.3338 0.02236 0.01714 -0.0976 0.2896 0.8880
9.750 1.3357 0.02642 0.02110 -0.0940 0.2438 0.9085
10.000 1.3419 0.02838 0.02305 -0.0933 0.2230 0.9320
11.000 1.3444 0.03776 0.03200 -0.0871 0.1256 1.0000
11.250 1.3381 0.04051 0.03456 -0.0848 0.0949 1.0000
11.500 1.3388 0.04275 0.03670 -0.0833 0.0771 1.0000
11.750 1.3506 0.04408 0.03806 -0.0826 0.0728 1.0000
12.000 1.3542 0.04612 0.04003 -0.0813 0.0589 1.0000
12.250 1.3590 0.04810 0.04196 -0.0802 0.0478 1.0000
12.500 1.3661 0.04988 0.04371 -0.0793 0.0399 1.0000
12.750 1.3715 0.05183 0.04564 -0.0783 0.0326 1.0000
13.000 1.3807 0.05346 0.04728 -0.0776 0.0296 1.0000
13.250 1.3906 0.05504 0.04888 -0.0769 0.0269 1.0000
13.500 1.3971 0.05697 0.05080 -0.0761 0.0231 1.0000
13.750 1.4067 0.05861 0.05247 -0.0756 0.0216 1.0000
14.000 1.4164 0.06023 0.05413 -0.0750 0.0198 1.0000
14.250 1.4233 0.06216 0.05607 -0.0744 0.0175 1.0000
14.500 1.4322 0.06388 0.05783 -0.0738 0.0164 1.0000
14.750 1.4418 0.06555 0.05954 -0.0734 0.0158 1.0000
15.000 1.4481 0.06757 0.06158 -0.0728 0.0135 1.0000
15.250 1.4560 0.06947 0.06352 -0.0723 0.0131 1.0000
15.500 1.4633 0.07139 0.06548 -0.0719 0.0109 1.0000
15.750 1.4699 0.07343 0.06755 -0.0714 0.0099 1.0000
16.000 1.4752 0.07564 0.06979 -0.0709 0.0082 1.0000
16.250 1.4782 0.07804 0.07219 -0.0704 0.0058 1.0000
16.500 1.4830 0.08033 0.07453 -0.0700 0.0052 1.0000
16.750 1.4879 0.08263 0.07688 -0.0697 0.0046 1.0000
17.000 1.4940 0.08478 0.07910 -0.0694 0.0045 1.0000
17.250 1.4963 0.08744 0.08180 -0.0691 0.0039 1.0000
17.500 1.5004 0.08986 0.08428 -0.0689 0.0037 1.0000
17.750 1.5043 0.09232 0.08681 -0.0687 0.0033 1.0000
18.000 1.5073 0.09491 0.08947 -0.0686 0.0031 1.0000
18.250 1.5114 0.09737 0.09199 -0.0685 0.0030 1.0000
18.500 1.5125 0.10026 0.09495 -0.0685 0.0029 1.0000
18.750 1.5151 0.10296 0.09771 -0.0685 0.0028 1.0000
19.000 1.5151 0.10602 0.10084 -0.0687 0.0026 1.0000
19.250 1.5178 0.10875 0.10365 -0.0689 0.0026 1.0000
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