USA 34 AIRFOIL (usa34-il)
USA 34 AIRFOIL - USA-34 airfoil
| Details | Dat file | Parser | |
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(usa34-il) USA 34 AIRFOIL USA-34 airfoil Max thickness 18% at 29.5% chord. Max camber 7.7% at 39.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
USA 34 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0110100 0.0433500
0.0229800 0.0597400
0.0472500 0.0825200
0.0717500 0.0983100
0.0963100 0.1121000
0.1456900 0.1316700
0.1952200 0.1462600
0.2947200 0.1624500
0.3947000 0.1636500
0.4950200 0.1538600
0.5955700 0.1370700
0.6964400 0.1103000
0.7974700 0.0785300
0.8985900 0.0437600
0.9492100 0.0243800
1.0000000 0.0000000
0.0000000 0.0000000
0.0128600 -.0145900
0.0255600 -.0211900
0.0508600 -.0303800
0.0759500 -.0330800
0.1009900 -.0337800
0.1509000 -.0311800
0.2007900 -.0275800
0.3004800 -.0173900
0.4002300 -.0091900
0.5001000 -.0050000
0.6000400 -.0028000
0.7000500 -.0026000
0.8000801 -.0034000
0.9001300 -.0042000
0.9501400 -.0046000
1.0000000 0.0000000
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Polars for USA 34 AIRFOIL (usa34-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| usa34-il | 50,000 | 9 | 4 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa34-il | 50,000 | 5 | 9.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa34-il | 100,000 | 9 | 9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa34-il | 100,000 | 5 | 40.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa34-il | 200,000 | 9 | 66.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa34-il | 200,000 | 5 | 60.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa34-il | 500,000 | 9 | 86.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa34-il | 500,000 | 5 | 75 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa34-il | 1,000,000 | 9 | 104.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa34-il | 1,000,000 | 5 | 87.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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