RAF 28 AIRFOIL (raf28-il)
RAF 28 AIRFOIL - RAF-28 airfoil
| Details | Dat file | Parser | |
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(raf28-il) RAF 28 AIRFOIL RAF-28 airfoil Max thickness 9.8% at 30% chord. Max camber 1.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RAF 28 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0145000
0.0250000 0.0210000
0.0500000 0.0313000
0.0750000 0.0390000
0.1000000 0.0446000
0.1500000 0.0536000
0.2000000 0.0600000
0.3000000 0.0670000
0.4000000 0.0672000
0.5000000 0.0625000
0.6000000 0.0540000
0.7000000 0.0432000
0.8000000 0.0293000
0.9000000 0.0163000
0.9500000 0.0089000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0125000
0.0250000 -.0165000
0.0500000 -.0220000
0.0750000 -.0253000
0.1000000 -.0275000
0.1500000 -.0305000
0.2000000 -.0320000
0.3000000 -.0312000
0.4000000 -.0286000
0.5000000 -.0250000
0.6000000 -.0210000
0.7000000 -.0160000
0.8000000 -.0110000
0.9000000 -.0063000
0.9500000 -.0034000
1.0000000 0.0000000
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Polars for RAF 28 AIRFOIL (raf28-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| raf28-il | 50,000 | 9 | 35.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf28-il | 50,000 | 5 | 35.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf28-il | 100,000 | 9 | 52.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf28-il | 100,000 | 5 | 50.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf28-il | 200,000 | 9 | 69.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf28-il | 200,000 | 5 | 64.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf28-il | 500,000 | 9 | 90.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf28-il | 500,000 | 5 | 79.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf28-il | 1,000,000 | 9 | 103.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf28-il | 1,000,000 | 5 | 83.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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