RAF 33 AIRFOIL (raf33-il)
RAF 33 AIRFOIL - RAF-33 airfoil
| Details | Dat file | Parser | |
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(raf33-il) RAF 33 AIRFOIL RAF-33 airfoil Max thickness 12.6% at 30% chord. Max camber 4.7% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RAF 33 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125500 0.0227700
0.0250800 0.0339400
0.0501200 0.0502800
0.0751500 0.0629200
0.1001800 0.0745600
0.1502200 0.0910400
0.2002400 0.1011200
0.3002600 0.1100800
0.4002600 0.1070400
0.5002300 0.0940000
0.6001800 0.0741600
0.7001200 0.0519200
0.8000700 0.0296800
0.9000300 0.0114400
0.9500100 0.0059200
1.0000000 0.0000000
0.0000000 0.0000000
0.0124600 -.0150300
0.0249600 -.0186600
0.0499500 -.0207200
0.0749500 -.0211800
0.0999500 -.0208400
0.1499500 -.0197600
0.1999600 -.0184800
0.2999600 -.0163200
0.3999600 -.0173600
0.4999500 -.0200000
0.5999500 -.0220400
0.6999500 -.0226800
0.7999500 -.0209200
0.8999700 -.0139600
0.9499800 -.0088800
1.0000000 0.0000000
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Polars for RAF 33 AIRFOIL (raf33-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| raf33-il | 50,000 | 9 | 6.6 at α=-5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf33-il | 50,000 | 5 | 19.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf33-il | 100,000 | 9 | 39 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf33-il | 100,000 | 5 | 48.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf33-il | 200,000 | 9 | 71.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf33-il | 200,000 | 5 | 73.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf33-il | 500,000 | 9 | 107.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf33-il | 500,000 | 5 | 99.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf33-il | 1,000,000 | 9 | 127.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf33-il | 1,000,000 | 5 | 110.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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