NACA 0012-34 (naca001234-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0012-34 (naca001234-il) Reynolds number: 1,000,000 Max Cl/Cd: 55.74 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca001234-il-1000000-n5.txt Download as CSV file: xf-naca001234-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0012-34
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
------ -------- --------- --------- -------- -------- --------
-14.250 -0.9006 0.07344 0.07156 -0.0322 1.0000 0.0020
-14.000 -0.9307 0.06357 0.06150 -0.0386 1.0000 0.0020
-13.750 -0.9559 0.05608 0.05381 -0.0424 1.0000 0.0020
-13.500 -0.9761 0.05032 0.04785 -0.0442 1.0000 0.0020
-13.250 -0.9946 0.04542 0.04273 -0.0446 1.0000 0.0020
-13.000 -1.0093 0.04142 0.03851 -0.0439 1.0000 0.0020
-12.750 -1.0199 0.03815 0.03503 -0.0423 1.0000 0.0020
-12.500 -1.0267 0.03543 0.03210 -0.0403 1.0000 0.0020
-12.250 -1.0410 0.03209 0.02847 -0.0369 1.0000 0.0020
-12.000 -1.0475 0.02959 0.02571 -0.0336 1.0000 0.0021
-11.750 -1.0477 0.02774 0.02368 -0.0305 1.0000 0.0021
-11.500 -1.0446 0.02629 0.02207 -0.0275 1.0000 0.0022
-11.250 -1.0401 0.02515 0.02080 -0.0243 1.0000 0.0022
-11.000 -1.0371 0.02425 0.01979 -0.0204 1.0000 0.0023
-10.750 -1.0345 0.02352 0.01896 -0.0162 1.0000 0.0023
-10.500 -1.0294 0.02273 0.01807 -0.0125 1.0000 0.0024
-10.250 -1.0112 0.02181 0.01704 -0.0116 0.9989 0.0024
-10.000 -0.9884 0.02080 0.01591 -0.0116 0.9972 0.0025
-9.750 -0.9645 0.01984 0.01480 -0.0118 0.9957 0.0026
-9.500 -0.9396 0.01899 0.01386 -0.0121 0.9944 0.0027
-9.250 -0.9157 0.01818 0.01295 -0.0121 0.9921 0.0029
-9.000 -0.8905 0.01741 0.01208 -0.0123 0.9901 0.0031
-8.750 -0.8643 0.01666 0.01123 -0.0127 0.9884 0.0032
-8.500 -0.8377 0.01594 0.01042 -0.0131 0.9868 0.0034
-8.250 -0.8142 0.01515 0.00953 -0.0128 0.9839 0.0035
-8.000 -0.7917 0.01430 0.00860 -0.0124 0.9803 0.0037
-7.750 -0.7655 0.01375 0.00801 -0.0126 0.9777 0.0040
-7.500 -0.7398 0.01328 0.00749 -0.0126 0.9746 0.0042
-7.250 -0.7161 0.01284 0.00698 -0.0121 0.9701 0.0045
-7.000 -0.6906 0.01240 0.00649 -0.0120 0.9664 0.0049
-6.750 -0.6662 0.01200 0.00603 -0.0117 0.9622 0.0052
-6.500 -0.6420 0.01167 0.00566 -0.0112 0.9571 0.0055
-6.250 -0.6181 0.01121 0.00515 -0.0107 0.9526 0.0063
-6.000 -0.5938 0.01090 0.00483 -0.0102 0.9475 0.0070
-5.750 -0.5692 0.01061 0.00449 -0.0098 0.9420 0.0077
-5.500 -0.5438 0.01035 0.00417 -0.0095 0.9373 0.0083
-5.250 -0.5196 0.01003 0.00381 -0.0089 0.9313 0.0103
-5.000 -0.4946 0.00977 0.00355 -0.0086 0.9257 0.0127
-4.750 -0.4690 0.00955 0.00330 -0.0083 0.9200 0.0171
-4.500 -0.4437 0.00932 0.00307 -0.0080 0.9136 0.0247
-4.250 -0.4189 0.00903 0.00282 -0.0076 0.9075 0.0415
-4.000 -0.3954 0.00862 0.00257 -0.0070 0.9003 0.0815
-3.750 -0.3729 0.00813 0.00228 -0.0062 0.8933 0.1435
-3.500 -0.3518 0.00753 0.00201 -0.0053 0.8853 0.2303
-3.250 -0.3318 0.00686 0.00174 -0.0041 0.8774 0.3389
-3.000 -0.3099 0.00639 0.00155 -0.0032 0.8691 0.4181
-2.750 -0.2867 0.00603 0.00140 -0.0025 0.8605 0.4824
-2.500 -0.2625 0.00579 0.00128 -0.0020 0.8517 0.5285
-2.250 -0.2387 0.00554 0.00117 -0.0013 0.8418 0.5798
-2.000 -0.2131 0.00540 0.00109 -0.0010 0.8322 0.6106
-1.750 -0.1869 0.00530 0.00103 -0.0008 0.8233 0.6334
-1.500 -0.1604 0.00523 0.00097 -0.0007 0.8139 0.6533
-1.250 -0.1340 0.00515 0.00093 -0.0005 0.8047 0.6742
-1.000 -0.1076 0.00509 0.00090 -0.0003 0.7955 0.6960
-0.750 -0.0810 0.00505 0.00087 -0.0002 0.7856 0.7137
-0.500 -0.0540 0.00502 0.00086 -0.0001 0.7754 0.7284
-0.250 -0.0270 0.00501 0.00085 -0.0001 0.7649 0.7415
0.000 0.0000 0.00500 0.00084 0.0000 0.7537 0.7537
0.250 0.0270 0.00501 0.00085 0.0001 0.7415 0.7649
0.500 0.0540 0.00502 0.00086 0.0001 0.7284 0.7755
0.750 0.0810 0.00505 0.00087 0.0002 0.7137 0.7856
1.000 0.1076 0.00509 0.00090 0.0003 0.6960 0.7956
1.250 0.1340 0.00515 0.00093 0.0005 0.6743 0.8048
1.500 0.1604 0.00523 0.00097 0.0007 0.6530 0.8139
1.750 0.1870 0.00530 0.00103 0.0008 0.6334 0.8232
2.000 0.2131 0.00540 0.00109 0.0010 0.6107 0.8322
2.250 0.2387 0.00553 0.00117 0.0013 0.5804 0.8418
2.500 0.2625 0.00578 0.00128 0.0020 0.5288 0.8517
2.750 0.2868 0.00604 0.00140 0.0025 0.4819 0.8605
3.000 0.3100 0.00639 0.00155 0.0032 0.4191 0.8691
3.250 0.3317 0.00688 0.00175 0.0042 0.3352 0.8774
3.500 0.3519 0.00753 0.00201 0.0053 0.2306 0.8853
3.750 0.3730 0.00813 0.00228 0.0062 0.1436 0.8933
4.000 0.3955 0.00862 0.00256 0.0070 0.0817 0.9002
4.250 0.4190 0.00903 0.00282 0.0076 0.0415 0.9074
4.500 0.4438 0.00932 0.00307 0.0080 0.0247 0.9135
4.750 0.4691 0.00955 0.00330 0.0083 0.0170 0.9198
5.000 0.4946 0.00977 0.00355 0.0086 0.0127 0.9255
5.250 0.5197 0.01003 0.00381 0.0089 0.0103 0.9312
5.500 0.5440 0.01035 0.00417 0.0095 0.0083 0.9373
5.750 0.5694 0.01061 0.00449 0.0098 0.0077 0.9419
6.000 0.5940 0.01090 0.00482 0.0102 0.0070 0.9474
6.250 0.6182 0.01121 0.00515 0.0107 0.0063 0.9526
6.500 0.6421 0.01168 0.00567 0.0112 0.0054 0.9570
6.750 0.6664 0.01200 0.00603 0.0116 0.0052 0.9622
7.000 0.6909 0.01240 0.00648 0.0120 0.0048 0.9664
7.250 0.7163 0.01285 0.00699 0.0121 0.0045 0.9700
7.500 0.7400 0.01328 0.00749 0.0126 0.0042 0.9747
7.750 0.7657 0.01376 0.00802 0.0125 0.0040 0.9777
8.000 0.7919 0.01431 0.00860 0.0123 0.0038 0.9804
8.250 0.8144 0.01515 0.00953 0.0128 0.0035 0.9840
8.500 0.8381 0.01593 0.01041 0.0130 0.0034 0.9869
8.750 0.8647 0.01665 0.01123 0.0126 0.0032 0.9885
9.000 0.8909 0.01741 0.01208 0.0122 0.0031 0.9901
9.250 0.9161 0.01819 0.01296 0.0120 0.0029 0.9921
9.500 0.9402 0.01898 0.01384 0.0119 0.0027 0.9944
9.750 0.9652 0.01984 0.01481 0.0116 0.0026 0.9958
10.000 0.9889 0.02082 0.01594 0.0115 0.0025 0.9973
10.250 1.0117 0.02183 0.01706 0.0115 0.0024 0.9989
10.500 1.0292 0.02273 0.01807 0.0126 0.0024 1.0000
10.750 1.0347 0.02352 0.01896 0.0162 0.0023 1.0000
11.000 1.0374 0.02427 0.01981 0.0204 0.0023 1.0000
11.250 1.0403 0.02519 0.02084 0.0242 0.0022 1.0000
11.500 1.0450 0.02632 0.02210 0.0274 0.0022 1.0000
11.750 1.0483 0.02777 0.02370 0.0304 0.0021 1.0000
12.000 1.0478 0.02965 0.02578 0.0335 0.0021 1.0000
12.250 1.0418 0.03212 0.02850 0.0368 0.0020 1.0000
12.500 1.0280 0.03541 0.03209 0.0401 0.0020 1.0000
12.750 1.0198 0.03829 0.03518 0.0422 0.0020 1.0000
13.000 1.0099 0.04150 0.03860 0.0437 0.0020 1.0000
13.250 0.9961 0.04541 0.04272 0.0444 0.0020 1.0000
13.500 0.9776 0.05032 0.04786 0.0440 0.0020 1.0000
13.750 0.9557 0.05634 0.05408 0.0420 0.0020 1.0000
14.000 0.9297 0.06406 0.06200 0.0380 0.0020 1.0000
14.250 0.8997 0.07403 0.07216 0.0315 0.0020 1.0000
14.500 0.8029 0.10484 0.10334 0.0156 0.0022 1.0000
14.750 0.8285 0.10283 0.10129 0.0154 0.0021 1.0000
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