12% JOUKOWSKI AIRFOIL (joukowsk-il)
12% JOUKOWSKI AIRFOIL - 12% Joukowski airfoil
| Details | Dat file | Parser | |
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(joukowsk-il) 12% JOUKOWSKI AIRFOIL 12% Joukowski airfoil Max thickness 11.8% at 25% chord. Max camber 0% at 9.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
12% JOUKOWSKI AIRFOIL
46.0 46.0
0.0000000 0.0000000
0.0012180 0.0063290
0.0048660 0.0125800
0.0109260 0.0186800
0.0193690 0.0245530
0.0301540 0.0301310
0.0432270 0.0353490
0.0585260 0.0401490
0.0759760 0.0444790
0.0954910 0.0482940
0.1169780 0.0515580
0.1403300 0.0542450
0.1654350 0.0563370
0.1921690 0.0578250
0.2204040 0.0587090
0.2500000 0.0590000
0.2808140 0.0587170
0.3126970 0.0578860
0.3454910 0.0565430
0.3790390 0.0547300
0.4131760 0.0524950
0.4477360 0.0498910
0.4825500 0.0469750
0.5174500 0.0438060
0.5522640 0.0404480
0.5868240 0.0369610
0.6209610 0.0334080
0.6545080 0.0298470
0.6873030 0.0263360
0.7191850 0.0229270
0.7500000 0.0196670
0.7795960 0.0165980
0.8078310 0.0137550
0.8345650 0.0111680
0.8596700 0.0088550
0.8830220 0.0068300
0.9045080 0.0050990
0.9240240 0.0036570
0.9414740 0.0024960
0.9567730 0.0015970
0.9698460 0.0009370
0.9806310 0.0004850
0.9890740 0.0002060
0.9951340 0.0000620
0.9987820 0.0000080
1.0000000 0.0000000
0.0000000 0.0000000
0.0012180 -.0063290
0.0048660 -.0125800
0.0109260 -.0186800
0.0193690 -.0245530
0.0301540 -.0301310
0.0432270 -.0353490
0.0585260 -.0401490
0.0759760 -.0444790
0.0954920 -.0482940
0.1169780 -.0515580
0.1403300 -.0542450
0.1654350 -.0563370
0.1921690 -.0578250
0.2204040 -.0587090
0.2500000 -.0590000
0.2808140 -.0587170
0.3126970 -.0578860
0.3454910 -.0565430
0.3790390 -.0547300
0.4131760 -.0524950
0.4477360 -.0498910
0.4825500 -.0469750
0.5174500 -.0438060
0.5522640 -.0404480
0.5868240 -.0369610
0.6209610 -.0334080
0.6545090 -.0298470
0.6873030 -.0263360
0.7191850 -.0229270
0.7500000 -.0196670
0.7795960 -.0165980
0.8078310 -.0137550
0.8345650 -.0111680
0.8596700 -.0088550
0.8830220 -.0068300
0.9045090 -.0050990
0.9240240 -.0036570
0.9414740 -.0024960
0.9567730 -.0015970
0.9698460 -.0009370
0.9806310 -.0004850
0.9890740 -.0002060
0.9951340 -.0000620
0.9987820 -.0000080
1.0000000 0.0000000
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Polars for 12% JOUKOWSKI AIRFOIL (joukowsk-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| joukowsk-il | 50,000 | 9 | 22.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 50,000 | 5 | 26.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 100,000 | 9 | 34.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 100,000 | 5 | 37.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 200,000 | 9 | 47.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 200,000 | 5 | 48.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 500,000 | 9 | 65.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 500,000 | 5 | 65.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk-il | 1,000,000 | 9 | 80.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk-il | 1,000,000 | 5 | 79.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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