Joukovsky f=0% t=15% (joukowsk0015-jf) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: Joukovsky f=0% t=15% (joukowsk0015-jf) Reynolds number: 100,000 Max Cl/Cd: 37.96 at α=7.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-joukowsk0015-jf-100000-n5.txt Download as CSV file: xf-joukowsk0015-jf-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Joukovsky f=0% t=15%
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
------ -------- --------- --------- -------- -------- --------
-16.250 -0.9736 0.11163 0.10536 0.0074 1.0000 0.0660
-16.000 -1.0380 0.09494 0.08829 -0.0035 1.0000 0.0666
-15.750 -1.0245 0.09369 0.08712 -0.0035 1.0000 0.0680
-15.500 -1.0384 0.08744 0.08075 -0.0072 1.0000 0.0691
-15.250 -1.0554 0.08092 0.07406 -0.0110 1.0000 0.0702
-15.000 -1.0716 0.07485 0.06780 -0.0144 1.0000 0.0714
-14.750 -1.0862 0.06928 0.06201 -0.0174 1.0000 0.0726
-14.500 -1.1002 0.06403 0.05649 -0.0201 1.0000 0.0740
-14.250 -1.0971 0.06137 0.05385 -0.0209 1.0000 0.0755
-14.000 -1.0964 0.05845 0.05089 -0.0220 1.0000 0.0771
-13.750 -1.0981 0.05528 0.04762 -0.0231 1.0000 0.0789
-13.500 -1.1003 0.05209 0.04426 -0.0241 1.0000 0.0808
-13.250 -1.1019 0.04904 0.04102 -0.0249 1.0000 0.0828
-13.000 -1.0968 0.04695 0.03896 -0.0251 1.0000 0.0847
-12.750 -1.0932 0.04476 0.03671 -0.0253 1.0000 0.0869
-12.500 -1.0902 0.04254 0.03438 -0.0254 1.0000 0.0895
-12.250 -1.0865 0.04041 0.03208 -0.0253 1.0000 0.0922
-12.000 -1.0800 0.03873 0.03043 -0.0249 1.0000 0.0945
-11.750 -1.0740 0.03708 0.02874 -0.0244 1.0000 0.0974
-11.500 -1.0673 0.03550 0.02701 -0.0237 1.0000 0.1009
-11.250 -1.0598 0.03409 0.02558 -0.0227 1.0000 0.1039
-11.000 -1.0520 0.03284 0.02433 -0.0215 1.0000 0.1072
-10.750 -1.0427 0.03169 0.02308 -0.0201 1.0000 0.1114
-10.500 -1.0313 0.03059 0.02196 -0.0189 1.0000 0.1154
-10.250 -1.0177 0.02958 0.02093 -0.0178 1.0000 0.1200
-10.000 -1.0019 0.02860 0.01984 -0.0169 1.0000 0.1256
-9.750 -0.9865 0.02766 0.01896 -0.0159 1.0000 0.1306
-9.500 -0.9685 0.02681 0.01799 -0.0151 1.0000 0.1371
-9.250 -0.9510 0.02595 0.01719 -0.0143 1.0000 0.1430
-9.000 -0.9313 0.02518 0.01634 -0.0135 1.0000 0.1505
-8.750 -0.9121 0.02440 0.01563 -0.0128 1.0000 0.1574
-8.500 -0.8909 0.02372 0.01486 -0.0122 1.0000 0.1660
-8.250 -0.8705 0.02302 0.01423 -0.0115 1.0000 0.1739
-8.000 -0.8487 0.02238 0.01358 -0.0110 1.0000 0.1831
-7.750 -0.8267 0.02178 0.01299 -0.0104 1.0000 0.1927
-7.500 -0.8045 0.02120 0.01245 -0.0098 1.0000 0.2024
-7.250 -0.7815 0.02067 0.01190 -0.0093 1.0000 0.2133
-7.000 -0.7589 0.02015 0.01143 -0.0088 1.0000 0.2241
-6.750 -0.7360 0.01967 0.01100 -0.0083 1.0000 0.2350
-6.500 -0.7130 0.01923 0.01057 -0.0077 1.0000 0.2469
-6.250 -0.6909 0.01882 0.01021 -0.0071 1.0000 0.2587
-6.000 -0.6702 0.01843 0.00990 -0.0062 1.0000 0.2702
-5.750 -0.6380 0.01807 0.00958 -0.0075 0.9821 0.2843
-5.500 -0.5995 0.01775 0.00926 -0.0098 0.9598 0.2999
-5.250 -0.5622 0.01747 0.00897 -0.0117 0.9394 0.3157
-5.000 -0.5288 0.01723 0.00873 -0.0127 0.9188 0.3305
-4.750 -0.4991 0.01702 0.00855 -0.0129 0.8981 0.3444
-4.500 -0.4718 0.01684 0.00836 -0.0125 0.8784 0.3581
-4.250 -0.4459 0.01668 0.00817 -0.0119 0.8596 0.3720
-4.000 -0.4206 0.01654 0.00798 -0.0110 0.8417 0.3861
-3.750 -0.3956 0.01640 0.00786 -0.0101 0.8247 0.3992
-3.500 -0.3705 0.01627 0.00771 -0.0092 0.8085 0.4126
-3.250 -0.3451 0.01616 0.00755 -0.0083 0.7929 0.4267
-3.000 -0.3193 0.01604 0.00742 -0.0076 0.7768 0.4406
-2.750 -0.2934 0.01593 0.00733 -0.0068 0.7612 0.4538
-2.500 -0.2673 0.01584 0.00721 -0.0061 0.7464 0.4674
-2.250 -0.2412 0.01576 0.00708 -0.0054 0.7322 0.4818
-2.000 -0.2148 0.01568 0.00701 -0.0047 0.7173 0.4952
-1.750 -0.1881 0.01561 0.00696 -0.0041 0.7026 0.5086
-1.500 -0.1614 0.01555 0.00687 -0.0035 0.6886 0.5225
-1.250 -0.1347 0.01551 0.00678 -0.0028 0.6752 0.5368
-1.000 -0.1078 0.01547 0.00678 -0.0023 0.6603 0.5498
-0.750 -0.0809 0.01543 0.00674 -0.0017 0.6463 0.5635
-0.500 -0.0539 0.01542 0.00668 -0.0011 0.6330 0.5779
-0.250 -0.0270 0.01540 0.00668 -0.0005 0.6189 0.5914
0.000 0.0000 0.01539 0.00670 0.0000 0.6046 0.6046
0.250 0.0270 0.01540 0.00668 0.0005 0.5914 0.6189
0.500 0.0539 0.01542 0.00668 0.0011 0.5779 0.6330
0.750 0.0809 0.01543 0.00674 0.0017 0.5635 0.6463
1.000 0.1078 0.01547 0.00678 0.0023 0.5498 0.6603
1.250 0.1347 0.01551 0.00678 0.0028 0.5368 0.6753
1.500 0.1614 0.01555 0.00687 0.0035 0.5225 0.6886
1.750 0.1881 0.01561 0.00696 0.0041 0.5086 0.7026
2.000 0.2148 0.01568 0.00701 0.0047 0.4952 0.7174
2.250 0.2412 0.01576 0.00708 0.0054 0.4818 0.7323
2.500 0.2673 0.01584 0.00721 0.0061 0.4674 0.7464
2.750 0.2934 0.01593 0.00733 0.0068 0.4538 0.7612
3.000 0.3193 0.01604 0.00742 0.0076 0.4406 0.7768
3.250 0.3451 0.01616 0.00755 0.0083 0.4266 0.7929
3.500 0.3705 0.01627 0.00771 0.0092 0.4126 0.8085
3.750 0.3956 0.01640 0.00786 0.0101 0.3992 0.8247
4.000 0.4206 0.01654 0.00798 0.0110 0.3861 0.8417
4.250 0.4459 0.01668 0.00817 0.0118 0.3720 0.8596
4.500 0.4718 0.01684 0.00836 0.0125 0.3581 0.8784
4.750 0.4991 0.01702 0.00855 0.0129 0.3445 0.8981
5.000 0.5288 0.01723 0.00873 0.0127 0.3305 0.9188
5.250 0.5622 0.01747 0.00897 0.0117 0.3157 0.9394
5.500 0.5995 0.01775 0.00926 0.0098 0.2999 0.9598
5.750 0.6380 0.01807 0.00958 0.0075 0.2843 0.9821
6.000 0.6702 0.01843 0.00990 0.0062 0.2702 1.0000
6.250 0.6909 0.01882 0.01021 0.0071 0.2588 1.0000
6.500 0.7130 0.01923 0.01057 0.0077 0.2470 1.0000
6.750 0.7361 0.01967 0.01100 0.0083 0.2350 1.0000
7.000 0.7589 0.02015 0.01143 0.0088 0.2240 1.0000
7.250 0.7815 0.02067 0.01190 0.0093 0.2133 1.0000
7.500 0.8045 0.02120 0.01245 0.0098 0.2024 1.0000
7.750 0.8268 0.02178 0.01298 0.0104 0.1927 1.0000
8.000 0.8487 0.02238 0.01358 0.0109 0.1831 1.0000
8.250 0.8706 0.02302 0.01423 0.0115 0.1739 1.0000
8.500 0.8909 0.02372 0.01486 0.0122 0.1660 1.0000
8.750 0.9121 0.02440 0.01563 0.0128 0.1573 1.0000
9.000 0.9314 0.02518 0.01634 0.0135 0.1505 1.0000
9.250 0.9511 0.02595 0.01719 0.0142 0.1430 1.0000
9.500 0.9687 0.02681 0.01799 0.0151 0.1371 1.0000
9.750 0.9867 0.02766 0.01896 0.0159 0.1305 1.0000
10.000 1.0020 0.02860 0.01984 0.0169 0.1255 1.0000
10.250 1.0179 0.02958 0.02092 0.0178 0.1200 1.0000
10.500 1.0314 0.03059 0.02196 0.0189 0.1154 1.0000
10.750 1.0429 0.03169 0.02307 0.0201 0.1113 1.0000
11.000 1.0522 0.03284 0.02432 0.0215 0.1072 1.0000
11.250 1.0601 0.03408 0.02558 0.0227 0.1039 1.0000
11.500 1.0676 0.03550 0.02701 0.0237 0.1008 1.0000
11.750 1.0744 0.03708 0.02873 0.0244 0.0973 1.0000
12.000 1.0805 0.03872 0.03042 0.0249 0.0945 1.0000
12.250 1.0871 0.04040 0.03206 0.0253 0.0922 1.0000
12.500 1.0907 0.04253 0.03437 0.0254 0.0894 1.0000
12.750 1.0938 0.04474 0.03669 0.0253 0.0868 1.0000
13.000 1.0975 0.04693 0.03892 0.0250 0.0846 1.0000
13.250 1.1028 0.04901 0.04098 0.0248 0.0828 1.0000
13.500 1.1010 0.05208 0.04425 0.0240 0.0808 1.0000
13.750 1.0987 0.05527 0.04761 0.0230 0.0788 1.0000
14.000 1.0975 0.05840 0.05084 0.0219 0.0770 1.0000
14.250 1.0984 0.06129 0.05376 0.0209 0.0754 1.0000
14.500 1.1011 0.06403 0.05649 0.0200 0.0740 1.0000
14.750 1.0877 0.06920 0.06192 0.0174 0.0726 1.0000
15.000 1.0730 0.07480 0.06774 0.0143 0.0713 1.0000
15.250 1.0568 0.08085 0.07399 0.0109 0.0701 1.0000
15.500 1.0404 0.08730 0.08060 0.0071 0.0690 1.0000
15.750 1.0298 0.09293 0.08633 0.0039 0.0679 1.0000
16.000 1.0459 0.09373 0.08701 0.0042 0.0665 1.0000
16.250 0.9733 0.11200 0.10574 -0.0079 0.0660 1.0000
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