AG37 (ag37-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AG37 (ag37-il) Reynolds number: 1,000,000 Max Cl/Cd: 89.73 at α=3.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ag37-il-1000000-n5.txt Download as CSV file: xf-ag37-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AG37
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
------ -------- --------- --------- -------- -------- --------
-13.500 -0.5854 0.14722 0.14551 0.0231 1.0000 0.0046
-13.250 -0.5805 0.14343 0.14172 0.0216 1.0000 0.0047
-9.750 -0.6943 0.02339 0.02023 -0.0463 1.0000 0.0051
-9.500 -0.6770 0.02024 0.01665 -0.0457 1.0000 0.0053
-9.250 -0.6564 0.01836 0.01447 -0.0450 1.0000 0.0055
-9.000 -0.6347 0.01694 0.01282 -0.0442 1.0000 0.0056
-8.750 -0.6121 0.01583 0.01150 -0.0434 1.0000 0.0058
-8.500 -0.5849 0.01483 0.01032 -0.0435 0.9989 0.0059
-8.250 -0.5548 0.01396 0.00930 -0.0442 0.9972 0.0060
-8.000 -0.5236 0.01324 0.00846 -0.0450 0.9954 0.0061
-7.750 -0.4930 0.01217 0.00722 -0.0458 0.9935 0.0064
-7.500 -0.4634 0.01153 0.00648 -0.0462 0.9903 0.0066
-7.250 -0.4327 0.01108 0.00598 -0.0468 0.9870 0.0069
-7.000 -0.4010 0.01068 0.00552 -0.0476 0.9837 0.0072
-6.750 -0.3716 0.01032 0.00513 -0.0479 0.9791 0.0076
-6.500 -0.3417 0.00998 0.00474 -0.0482 0.9737 0.0081
-6.250 -0.3120 0.00966 0.00436 -0.0485 0.9674 0.0086
-6.000 -0.2837 0.00936 0.00401 -0.0484 0.9585 0.0088
-5.750 -0.2564 0.00890 0.00349 -0.0482 0.9484 0.0096
-5.500 -0.2296 0.00866 0.00322 -0.0478 0.9344 0.0102
-5.250 -0.2036 0.00847 0.00294 -0.0471 0.9116 0.0109
-5.000 -0.1797 0.00840 0.00266 -0.0459 0.8534 0.0116
-4.750 -0.1533 0.00836 0.00245 -0.0453 0.8185 0.0122
-4.500 -0.1261 0.00820 0.00218 -0.0450 0.7929 0.0138
-4.000 -0.0708 0.00806 0.00184 -0.0447 0.7454 0.0165
-3.750 -0.0430 0.00797 0.00166 -0.0446 0.7214 0.0187
-3.500 -0.0152 0.00791 0.00151 -0.0445 0.6916 0.0218
-3.250 0.0121 0.00797 0.00138 -0.0443 0.6285 0.0271
-3.000 0.0397 0.00800 0.00128 -0.0442 0.5923 0.0359
-2.750 0.0677 0.00795 0.00121 -0.0442 0.5707 0.0514
-2.500 0.0958 0.00784 0.00113 -0.0443 0.5545 0.0820
-2.250 0.1239 0.00771 0.00107 -0.0443 0.5408 0.1223
-2.000 0.1520 0.00752 0.00103 -0.0445 0.5291 0.1836
-1.750 0.1801 0.00731 0.00100 -0.0446 0.5181 0.2586
-1.500 0.2080 0.00703 0.00099 -0.0448 0.5075 0.3642
-1.250 0.2359 0.00677 0.00098 -0.0450 0.4971 0.4653
-1.000 0.2636 0.00645 0.00099 -0.0451 0.4871 0.5894
-0.750 0.2900 0.00602 0.00103 -0.0448 0.4768 0.7523
-0.500 0.3140 0.00573 0.00107 -0.0438 0.4649 0.8708
-0.250 0.3377 0.00559 0.00108 -0.0425 0.4510 0.9584
0.000 0.3739 0.00565 0.00107 -0.0443 0.4331 1.0000
0.250 0.4018 0.00577 0.00110 -0.0443 0.4147 1.0000
0.500 0.4296 0.00590 0.00114 -0.0443 0.3952 1.0000
0.750 0.4574 0.00605 0.00120 -0.0443 0.3759 1.0000
1.000 0.4852 0.00621 0.00126 -0.0444 0.3559 1.0000
1.250 0.5129 0.00638 0.00134 -0.0444 0.3367 1.0000
1.500 0.5406 0.00655 0.00142 -0.0444 0.3172 1.0000
1.750 0.5682 0.00673 0.00153 -0.0445 0.2965 1.0000
2.000 0.5958 0.00693 0.00163 -0.0445 0.2771 1.0000
2.250 0.6233 0.00713 0.00175 -0.0446 0.2559 1.0000
2.500 0.6507 0.00737 0.00188 -0.0446 0.2339 1.0000
2.750 0.6780 0.00761 0.00204 -0.0446 0.2112 1.0000
3.000 0.7052 0.00786 0.00220 -0.0447 0.1909 1.0000
3.250 0.7322 0.00816 0.00238 -0.0447 0.1670 1.0000
3.500 0.7591 0.00846 0.00259 -0.0447 0.1436 1.0000
3.750 0.7858 0.00877 0.00281 -0.0447 0.1228 1.0000
4.000 0.8126 0.00908 0.00304 -0.0447 0.1040 1.0000
4.250 0.8390 0.00945 0.00331 -0.0446 0.0845 1.0000
4.500 0.8656 0.00977 0.00358 -0.0446 0.0701 1.0000
4.750 0.8921 0.01010 0.00385 -0.0446 0.0580 1.0000
5.000 0.9184 0.01044 0.00414 -0.0445 0.0477 1.0000
5.250 0.9447 0.01077 0.00444 -0.0445 0.0400 1.0000
5.500 0.9712 0.01107 0.00474 -0.0444 0.0354 1.0000
5.750 0.9972 0.01142 0.00507 -0.0444 0.0298 1.0000
6.000 1.0235 0.01172 0.00539 -0.0443 0.0270 1.0000
6.250 1.0493 0.01209 0.00574 -0.0442 0.0238 1.0000
6.500 1.0752 0.01242 0.00612 -0.0441 0.0215 1.0000
6.750 1.1009 0.01277 0.00648 -0.0440 0.0196 1.0000
7.000 1.1261 0.01317 0.00689 -0.0438 0.0176 1.0000
7.250 1.1512 0.01359 0.00734 -0.0437 0.0160 1.0000
7.500 1.1765 0.01395 0.00775 -0.0435 0.0150 1.0000
7.750 1.2013 0.01436 0.00819 -0.0433 0.0137 1.0000
8.000 1.2255 0.01484 0.00869 -0.0431 0.0125 1.0000
8.250 1.2495 0.01535 0.00925 -0.0428 0.0115 1.0000
8.500 1.2737 0.01578 0.00973 -0.0425 0.0109 1.0000
8.750 1.2975 0.01625 0.01024 -0.0422 0.0101 1.0000
9.000 1.3206 0.01677 0.01082 -0.0419 0.0093 1.0000
9.250 1.3430 0.01740 0.01148 -0.0414 0.0085 1.0000
9.500 1.3652 0.01799 0.01215 -0.0409 0.0080 1.0000
9.750 1.3875 0.01855 0.01278 -0.0405 0.0077 1.0000
10.000 1.4092 0.01914 0.01344 -0.0399 0.0072 1.0000
10.250 1.4303 0.01978 0.01413 -0.0394 0.0066 1.0000
10.500 1.4503 0.02049 0.01490 -0.0387 0.0061 1.0000
10.750 1.4687 0.02136 0.01584 -0.0378 0.0056 1.0000
11.000 1.4878 0.02207 0.01665 -0.0370 0.0055 1.0000
11.250 1.5059 0.02285 0.01752 -0.0361 0.0052 1.0000
11.500 1.5229 0.02368 0.01844 -0.0351 0.0050 1.0000
11.750 1.5387 0.02457 0.01942 -0.0339 0.0047 1.0000
12.000 1.5529 0.02551 0.02045 -0.0326 0.0045 1.0000
12.250 1.5650 0.02654 0.02156 -0.0310 0.0043 1.0000
12.500 1.5723 0.02764 0.02276 -0.0287 0.0041 1.0000
12.750 1.5763 0.02895 0.02418 -0.0262 0.0039 1.0000
13.000 1.5773 0.03058 0.02593 -0.0239 0.0038 1.0000
13.250 1.5781 0.03241 0.02788 -0.0220 0.0037 1.0000
13.500 1.5793 0.03439 0.02999 -0.0208 0.0036 1.0000
13.750 1.5792 0.03675 0.03248 -0.0202 0.0036 1.0000
14.000 1.5773 0.03962 0.03549 -0.0202 0.0035 1.0000
14.250 1.5733 0.04307 0.03908 -0.0209 0.0034 1.0000
14.500 1.5668 0.04718 0.04333 -0.0223 0.0034 1.0000
14.750 1.5577 0.05214 0.04845 -0.0246 0.0034 1.0000
15.000 1.5455 0.05787 0.05433 -0.0275 0.0033 1.0000
15.250 1.5280 0.06450 0.06112 -0.0307 0.0033 1.0000
15.500 1.5060 0.07190 0.06868 -0.0342 0.0033 1.0000
15.750 1.4801 0.08010 0.07703 -0.0381 0.0033 1.0000
16.000 1.4496 0.08929 0.08638 -0.0423 0.0033 1.0000
16.250 1.4172 0.09911 0.09635 -0.0469 0.0034 1.0000
16.500 1.3815 0.10989 0.10727 -0.0519 0.0034 1.0000
16.750 1.3474 0.12077 0.11829 -0.0571 0.0035 1.0000
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