SOKOLOV AIRFOIL (sokolov-il)
SOKOLOV AIRFOIL - Sokolov R/C sailplane airfoil
| Details | Dat file | Parser | |
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(sokolov-il) SOKOLOV AIRFOIL Sokolov R/C sailplane airfoil Max thickness 7.1% at 25% chord. Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SOKOLOV AIRFOIL
18. 18.
0.0000000 0.0000000
0.0125000 0.0161100
0.0250000 0.0252300
0.0500000 0.0389500
0.0750000 0.0496800
0.1000000 0.0584000
0.1500000 0.0708500
0.2000000 0.0818000
0.2500000 0.0882500
0.3000000 0.0922000
0.4000000 0.0956000
0.5000000 0.0905000
0.6000000 0.0804000
0.7000000 0.0663000
0.8000000 0.0492000
0.9000000 0.0301000
0.9500000 0.0185500
1.0000000 0.0070000
0.0000000 0.0000000
0.0125000 -.0078900
0.0250000 -.0087700
0.0500000 -.0070500
0.0750000 -.0053300
0.1000000 -.0011000
0.1500000 0.0053500
0.2000000 0.0113000
0.2500000 0.0172500
0.3000000 0.0227000
0.4000000 0.0326000
0.5000000 0.0385000
0.6000000 0.0384000
0.7000000 0.0343000
0.8000000 0.0252000
0.9000000 0.0141000
0.9500000 0.0070500
1.0000000 0.0000000
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Polars for SOKOLOV AIRFOIL (sokolov-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sokolov-il | 50,000 | 9 | 44.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sokolov-il | 50,000 | 5 | 45.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sokolov-il | 100,000 | 9 | 68.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sokolov-il | 100,000 | 5 | 69.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sokolov-il | 200,000 | 9 | 92.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sokolov-il | 200,000 | 5 | 92 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sokolov-il | 500,000 | 9 | 124.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sokolov-il | 500,000 | 5 | 118.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sokolov-il | 1,000,000 | 9 | 146.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sokolov-il | 1,000,000 | 5 | 109.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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