USA 22 AIRFOIL (usa22-il)
USA 22 AIRFOIL - USA-22 airfoil
| Details | Dat file | Parser | |
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(usa22-il) USA 22 AIRFOIL USA-22 airfoil Max thickness 9.1% at 19.9% chord. Max camber 4.4% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
USA 22 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122500 0.0171800
0.0246000 0.0273600
0.0493700 0.0437200
0.0742000 0.0552800
0.0990700 0.0644400
0.1489000 0.0761600
0.1988000 0.0828800
0.2987300 0.0873300
0.3988000 0.0827800
0.4989200 0.0742300
0.5990900 0.0626900
0.6992900 0.0491400
0.7995000 0.0345900
0.8997400 0.0180500
0.9498600 0.0097700
1.0000000 0.0005000
0.0000000 0.0000000
0.0126200 -.0083200
0.0251600 -.0111400
0.0501900 -.0127700
0.0751900 -.0134100
0.1002000 -.0135500
0.1501600 -.0113200
0.2001200 -.0081000
0.2999900 0.0008500
0.3999200 0.0058000
0.4999200 0.0052500
0.5999300 0.0047000
0.6999400 0.0041500
0.7999600 0.0026000
0.8999800 0.0010500
0.9500000 -.0000200
1.0000000 -.0005000
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Polars for USA 22 AIRFOIL (usa22-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| usa22-il | 50,000 | 9 | 32.5 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa22-il | 50,000 | 5 | 37.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa22-il | 100,000 | 9 | 53.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa22-il | 100,000 | 5 | 55.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa22-il | 200,000 | 9 | 73 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa22-il | 200,000 | 5 | 73.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa22-il | 500,000 | 9 | 99.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa22-il | 500,000 | 5 | 96.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa22-il | 1,000,000 | 9 | 119.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa22-il | 1,000,000 | 5 | 112.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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