USA 45 M AIRFOIL (usa45m-il)
USA 45 M AIRFOIL - USA-45M airfoil
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(usa45m-il) USA 45 M AIRFOIL USA-45M airfoil Max thickness 11.6% at 30% chord. Max camber 3.3% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
USA 45 M AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0191600
0.0250000 0.0297300
0.0500000 0.0473500
0.0750000 0.0606800
0.1000000 0.0700000
0.1500000 0.0824500
0.2000000 0.0894000
0.3000000 0.0914000
0.4000000 0.0845000
0.5000000 0.0745000
0.6000000 0.0623000
0.7000000 0.0484000
0.8000000 0.0332000
0.9000000 0.0170000
0.9500000 0.0085500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0146400
0.0250000 -.0176800
0.0500000 -.0193500
0.0750000 -.0205300
0.1000000 -.0220000
0.1500000 -.0240500
0.2000000 -.0253000
0.3000000 -.0249000
0.4000000 -.0238000
0.5000000 -.0223000
0.6000000 -.0195000
0.7000000 -.0159000
0.8000000 -.0113000
0.9000000 -.0061000
0.9500000 -.0029500
1.0000000 0.0000000
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Polars for USA 45 M AIRFOIL (usa45m-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| usa45m-il | 50,000 | 9 | 20.4 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa45m-il | 50,000 | 5 | 29.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa45m-il | 100,000 | 9 | 45.1 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa45m-il | 100,000 | 5 | 48 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa45m-il | 200,000 | 9 | 65.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa45m-il | 200,000 | 5 | 66.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa45m-il | 500,000 | 9 | 93.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa45m-il | 500,000 | 5 | 90.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa45m-il | 1,000,000 | 9 | 115.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa45m-il | 1,000,000 | 5 | 108.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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