USA 46 AIRFOIL (usa46-il)
USA 46 AIRFOIL - USA-46 airfoil
| Details | Dat file | Parser | |
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(usa46-il) USA 46 AIRFOIL USA-46 airfoil Max thickness 6.5% at 20% chord. Max camber 2.2% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
USA 46 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124800 0.0110200
0.0249800 0.0170300
0.0499600 0.0253700
0.0749600 0.0321000
0.0999500 0.0370400
0.1499400 0.0448100
0.1999300 0.0492800
0.2999300 0.0524200
0.3999300 0.0521600
0.4999300 0.0477000
0.5999400 0.0414400
0.6999500 0.0332800
0.7999700 0.0234200
0.8999800 0.0125600
0.9499900 0.0069300
1.0000000 0.0000000
0.0000000 0.0000000
0.0125100 -.0099800
0.0250200 -.0139600
0.0500200 -.0176300
0.0750300 -.0192900
0.1000300 -.0198600
0.1500300 -.0181900
0.2000200 -.0161200
0.3000200 -.0125800
0.4000100 -.0088400
0.5000100 -.0050000
0.6000000 -.0011600
0.7000000 0.0025800
0.7999900 0.0057200
0.9000000 0.0035600
0.9500000 0.0013300
1.0000000 0.0000000
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Polars for USA 46 AIRFOIL (usa46-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| usa46-il | 50,000 | 9 | 38.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa46-il | 50,000 | 5 | 38.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa46-il | 100,000 | 9 | 52.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa46-il | 100,000 | 5 | 51.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa46-il | 200,000 | 9 | 69 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa46-il | 200,000 | 5 | 63.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa46-il | 500,000 | 9 | 86.4 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa46-il | 500,000 | 5 | 75.1 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa46-il | 1,000,000 | 9 | 97.3 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa46-il | 1,000,000 | 5 | 80.8 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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