FX 60-160 AIRFOIL (fx60160-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 60-160 AIRFOIL (fx60160-il) Reynolds number: 1,000,000 Max Cl/Cd: 102.83 at α=3° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx60160-il-1000000-n5.txt Download as CSV file: xf-fx60160-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 60-160 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
------ -------- --------- --------- -------- -------- --------
-18.750 -0.9843 0.07526 0.07245 -0.0844 1.0000 0.0096
-18.500 -1.0074 0.06838 0.06542 -0.0882 1.0000 0.0098
-18.250 -1.0244 0.06275 0.05967 -0.0911 1.0000 0.0098
-18.000 -1.0363 0.05815 0.05496 -0.0932 1.0000 0.0100
-17.750 -1.0468 0.05399 0.05068 -0.0949 1.0000 0.0101
-17.500 -1.0536 0.05054 0.04714 -0.0960 1.0000 0.0103
-17.250 -1.0588 0.04751 0.04402 -0.0966 1.0000 0.0105
-17.000 -1.0628 0.04483 0.04124 -0.0969 1.0000 0.0106
-16.750 -1.0676 0.04234 0.03866 -0.0967 1.0000 0.0108
-16.500 -1.0712 0.04018 0.03642 -0.0961 1.0000 0.0109
-16.250 -1.0725 0.03803 0.03420 -0.0959 0.9998 0.0111
-16.000 -1.0603 0.03592 0.03202 -0.0979 0.9990 0.0115
-15.750 -1.0453 0.03413 0.03018 -0.0997 0.9977 0.0120
-15.500 -1.0302 0.03244 0.02844 -0.1013 0.9958 0.0123
-15.250 -1.0156 0.03092 0.02685 -0.1025 0.9929 0.0127
-15.000 -1.0006 0.02944 0.02529 -0.1036 0.9902 0.0130
-14.750 -0.9824 0.02814 0.02392 -0.1049 0.9877 0.0135
-14.500 -0.9635 0.02686 0.02255 -0.1063 0.9855 0.0137
-14.250 -0.9431 0.02561 0.02123 -0.1079 0.9838 0.0140
-14.000 -0.9264 0.02451 0.02010 -0.1086 0.9803 0.0145
-13.750 -0.9061 0.02353 0.01909 -0.1095 0.9771 0.0149
-13.500 -0.8816 0.02265 0.01817 -0.1111 0.9747 0.0155
-13.250 -0.8547 0.02171 0.01718 -0.1132 0.9728 0.0158
-13.000 -0.8289 0.02091 0.01632 -0.1148 0.9697 0.0164
-12.750 -0.8026 0.02011 0.01545 -0.1165 0.9661 0.0168
-12.500 -0.7738 0.01934 0.01462 -0.1186 0.9628 0.0171
-12.250 -0.7430 0.01852 0.01373 -0.1211 0.9594 0.0174
-12.000 -0.7233 0.01767 0.01284 -0.1217 0.9520 0.0181
-11.750 -0.6977 0.01700 0.01212 -0.1230 0.9454 0.0185
-11.500 -0.6826 0.01647 0.01154 -0.1220 0.9357 0.0189
-11.250 -0.6637 0.01603 0.01104 -0.1213 0.9264 0.0193
-11.000 -0.6438 0.01561 0.01055 -0.1207 0.9142 0.0198
-10.750 -0.6245 0.01520 0.01006 -0.1198 0.8982 0.0202
-10.500 -0.6039 0.01489 0.00964 -0.1191 0.8781 0.0207
-10.250 -0.5844 0.01461 0.00922 -0.1180 0.8562 0.0211
-10.000 -0.5649 0.01435 0.00884 -0.1170 0.8371 0.0213
-9.750 -0.5457 0.01404 0.00842 -0.1159 0.8214 0.0217
-9.500 -0.5272 0.01363 0.00791 -0.1147 0.8087 0.0223
-9.250 -0.5058 0.01331 0.00755 -0.1140 0.7987 0.0229
-9.000 -0.4837 0.01304 0.00721 -0.1134 0.7900 0.0234
-8.750 -0.4608 0.01277 0.00689 -0.1129 0.7813 0.0239
-8.500 -0.4376 0.01251 0.00658 -0.1124 0.7741 0.0244
-8.250 -0.4138 0.01225 0.00627 -0.1120 0.7673 0.0249
-8.000 -0.3900 0.01202 0.00596 -0.1116 0.7609 0.0253
-7.750 -0.3653 0.01176 0.00566 -0.1113 0.7551 0.0258
-7.500 -0.3405 0.01155 0.00540 -0.1110 0.7490 0.0263
-7.250 -0.3153 0.01137 0.00516 -0.1108 0.7439 0.0266
-7.000 -0.2908 0.01103 0.00479 -0.1105 0.7391 0.0277
-6.750 -0.2656 0.01080 0.00452 -0.1103 0.7339 0.0285
-6.250 -0.2138 0.01041 0.00409 -0.1101 0.7248 0.0302
-6.000 -0.1875 0.01024 0.00389 -0.1100 0.7203 0.0310
-5.750 -0.1612 0.01009 0.00369 -0.1099 0.7158 0.0319
-5.500 -0.1346 0.00995 0.00352 -0.1099 0.7117 0.0327
-5.250 -0.1079 0.00977 0.00332 -0.1099 0.7077 0.0340
-5.000 -0.0812 0.00960 0.00314 -0.1098 0.7035 0.0357
-4.750 -0.0546 0.00947 0.00300 -0.1098 0.6992 0.0374
-4.500 -0.0275 0.00935 0.00285 -0.1098 0.6954 0.0390
-4.250 -0.0001 0.00924 0.00273 -0.1099 0.6915 0.0404
-4.000 0.0270 0.00911 0.00258 -0.1099 0.6871 0.0427
-3.750 0.0539 0.00900 0.00246 -0.1099 0.6828 0.0459
-3.500 0.0812 0.00890 0.00236 -0.1099 0.6787 0.0488
-3.250 0.1088 0.00881 0.00226 -0.1100 0.6741 0.0506
-3.000 0.1359 0.00871 0.00215 -0.1100 0.6693 0.0557
-2.750 0.1629 0.00863 0.00206 -0.1100 0.6649 0.0604
-2.500 0.1905 0.00851 0.00197 -0.1101 0.6606 0.0699
-2.250 0.2164 0.00819 0.00184 -0.1101 0.6560 0.1327
-2.000 0.2418 0.00785 0.00168 -0.1099 0.6516 0.1992
-1.750 0.2662 0.00729 0.00152 -0.1098 0.6475 0.3275
-1.500 0.2918 0.00690 0.00140 -0.1098 0.6430 0.4126
-1.250 0.3179 0.00668 0.00135 -0.1097 0.6381 0.4770
-1.000 0.3448 0.00659 0.00134 -0.1096 0.6338 0.5110
-0.750 0.3724 0.00653 0.00135 -0.1097 0.6290 0.5386
-0.500 0.3999 0.00652 0.00137 -0.1097 0.6238 0.5581
-0.250 0.4271 0.00654 0.00139 -0.1096 0.6189 0.5709
0.000 0.4551 0.00655 0.00142 -0.1097 0.6140 0.5842
0.250 0.4828 0.00657 0.00146 -0.1098 0.6088 0.5929
0.750 0.5378 0.00666 0.00155 -0.1097 0.5984 0.6131
1.000 0.5653 0.00672 0.00159 -0.1097 0.5923 0.6180
1.250 0.5923 0.00678 0.00164 -0.1097 0.5868 0.6220
1.500 0.6200 0.00683 0.00169 -0.1097 0.5813 0.6259
1.750 0.6469 0.00690 0.00175 -0.1096 0.5748 0.6300
2.000 0.6736 0.00698 0.00180 -0.1094 0.5653 0.6335
2.250 0.6993 0.00709 0.00187 -0.1091 0.5541 0.6366
2.500 0.7246 0.00720 0.00196 -0.1087 0.5421 0.6399
2.750 0.7497 0.00733 0.00205 -0.1082 0.5274 0.6435
3.000 0.7733 0.00752 0.00215 -0.1074 0.5060 0.6465
3.250 0.7957 0.00777 0.00229 -0.1065 0.4817 0.6493
3.500 0.8185 0.00799 0.00243 -0.1056 0.4612 0.6522
3.750 0.8411 0.00821 0.00258 -0.1047 0.4410 0.6548
4.000 0.8627 0.00848 0.00277 -0.1036 0.4194 0.6573
4.250 0.8840 0.00875 0.00295 -0.1025 0.3971 0.6596
4.500 0.9030 0.00911 0.00318 -0.1009 0.3685 0.6620
4.750 0.9183 0.00960 0.00347 -0.0987 0.3277 0.6642
5.000 0.9278 0.01021 0.00382 -0.0954 0.2778 0.6661
5.250 0.9287 0.01108 0.00435 -0.0905 0.2084 0.6682
5.500 0.9326 0.01192 0.00492 -0.0862 0.1520 0.6704
5.750 0.9326 0.01295 0.00563 -0.0814 0.0836 0.6726
6.000 0.9497 0.01331 0.00596 -0.0797 0.0727 0.6748
6.250 0.9675 0.01365 0.00629 -0.0780 0.0653 0.6769
6.500 0.9849 0.01401 0.00663 -0.0764 0.0585 0.6790
6.750 1.0028 0.01436 0.00696 -0.0749 0.0534 0.6809
7.000 1.0200 0.01472 0.00732 -0.0733 0.0490 0.6829
7.250 1.0372 0.01510 0.00770 -0.0717 0.0447 0.6849
7.500 1.0544 0.01547 0.00809 -0.0702 0.0421 0.6871
7.750 1.0707 0.01589 0.00851 -0.0685 0.0391 0.6894
8.000 1.0873 0.01633 0.00895 -0.0669 0.0368 0.6915
8.250 1.1041 0.01675 0.00939 -0.0655 0.0356 0.6937
8.500 1.1205 0.01720 0.00987 -0.0640 0.0343 0.6958
8.750 1.1363 0.01769 0.01038 -0.0624 0.0333 0.6976
9.000 1.1515 0.01821 0.01093 -0.0608 0.0323 0.6997
9.250 1.1660 0.01879 0.01153 -0.0592 0.0312 0.7019
9.500 1.1800 0.01940 0.01218 -0.0575 0.0302 0.7043
9.750 1.1945 0.02002 0.01284 -0.0560 0.0293 0.7066
10.000 1.2093 0.02064 0.01349 -0.0546 0.0290 0.7088
10.250 1.2241 0.02127 0.01416 -0.0533 0.0283 0.7110
10.500 1.2382 0.02197 0.01490 -0.0519 0.0278 0.7132
10.750 1.2517 0.02271 0.01569 -0.0505 0.0272 0.7157
11.000 1.2649 0.02349 0.01651 -0.0491 0.0264 0.7182
11.250 1.2774 0.02434 0.01740 -0.0478 0.0256 0.7208
11.500 1.2891 0.02527 0.01836 -0.0464 0.0246 0.7234
11.750 1.3002 0.02628 0.01940 -0.0450 0.0237 0.7261
12.250 1.3254 0.02813 0.02137 -0.0428 0.0223 0.7320
12.500 1.3373 0.02915 0.02244 -0.0417 0.0212 0.7354
12.750 1.3479 0.03028 0.02359 -0.0406 0.0194 0.7387
13.000 1.3582 0.03148 0.02482 -0.0395 0.0181 0.7420
13.250 1.3640 0.03304 0.02635 -0.0382 0.0120 0.7454
13.500 1.3683 0.03477 0.02811 -0.0368 0.0096 0.7495
13.750 1.3724 0.03659 0.02999 -0.0356 0.0083 0.7542
14.000 1.3768 0.03843 0.03189 -0.0345 0.0075 0.7591
14.250 1.3836 0.04009 0.03363 -0.0336 0.0071 0.7649
14.500 1.3907 0.04178 0.03540 -0.0328 0.0069 0.7714
14.750 1.3968 0.04358 0.03729 -0.0320 0.0066 0.7786
15.000 1.4018 0.04554 0.03934 -0.0313 0.0062 0.7880
15.250 1.4071 0.04748 0.04137 -0.0306 0.0061 0.8005
15.500 1.4113 0.04951 0.04353 -0.0299 0.0058 0.8222
15.750 1.4305 0.05214 0.04653 -0.0331 0.0056 0.9325
16.000 1.4397 0.05481 0.04928 -0.0343 0.0054 1.0000
16.250 1.4436 0.05715 0.05169 -0.0340 0.0052 1.0000
16.500 1.4471 0.05959 0.05420 -0.0338 0.0052 1.0000
16.750 1.4509 0.06205 0.05673 -0.0337 0.0050 1.0000
17.000 1.4544 0.06458 0.05933 -0.0336 0.0049 1.0000
17.250 1.4566 0.06732 0.06214 -0.0337 0.0048 1.0000
17.500 1.4588 0.07009 0.06499 -0.0339 0.0047 1.0000
17.750 1.4604 0.07296 0.06793 -0.0341 0.0047 1.0000
18.000 1.4615 0.07597 0.07102 -0.0344 0.0045 1.0000
18.250 1.4615 0.07918 0.07431 -0.0349 0.0045 1.0000
18.500 1.4618 0.08238 0.07759 -0.0354 0.0044 1.0000
18.750 1.4613 0.08575 0.08104 -0.0361 0.0043 1.0000
19.000 1.4593 0.08936 0.08474 -0.0369 0.0042 1.0000
19.250 1.4572 0.09308 0.08854 -0.0378 0.0042 1.0000
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