USA 32 AIRFOIL (usa32-il)
USA 32 AIRFOIL - USA-32 airfoil
| Details | Dat file | Parser | |
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(usa32-il) USA 32 AIRFOIL USA-32 airfoil Max thickness 14.7% at 19.8% chord. Max camber 9.3% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
USA 32 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120700 0.0391300
0.0243700 0.0572700
0.0491100 0.0805400
0.0739400 0.0968100
0.0987900 0.1100900
0.1485700 0.1296300
0.1984100 0.1441800
0.2982600 0.1582800
0.3982500 0.1593800
0.4983300 0.1514800
0.5985200 0.1345800
0.6987400 0.1146900
0.7990700 0.0847900
0.8994800 0.0468900
0.9497200 0.0254500
1.0000000 0.0000000
0.0000000 0.0000000
0.0126100 -.0098600
0.0251300 -.0117200
0.0501500 -.0134500
0.0751600 -.0141700
0.1001500 -.0139000
0.1501100 -.0103500
0.2000300 -.0028000
0.2998400 0.0143000
0.3997000 0.0274000
0.4997300 0.0245000
0.5998100 0.0176000
0.6999400 0.0057000
0.8000400 -.0032000
0.9000599 -.0051000
0.9500400 -.0035500
1.0000000 0.0000000
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Polars for USA 32 AIRFOIL (usa32-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| usa32-il | 50,000 | 9 | 4.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa32-il | 50,000 | 5 | 13.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa32-il | 100,000 | 9 | 39.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa32-il | 100,000 | 5 | 41 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa32-il | 200,000 | 9 | 64.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa32-il | 200,000 | 5 | 50.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa32-il | 500,000 | 9 | 68.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa32-il | 500,000 | 5 | 59.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa32-il | 1,000,000 | 9 | 76.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa32-il | 1,000,000 | 5 | 67.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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