SARATOV AIRFOIL (saratov-il)
SARATOV AIRFOIL - Saratov R/C sailplane airfoil
| Details | Dat file | Parser | |
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(saratov-il) SARATOV AIRFOIL Saratov R/C sailplane airfoil Max thickness 9.2% at 15% chord. Max camber 9.8% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SARATOV AIRFOIL
15. 15.
0.0000000 0.0000000
0.0125000 0.0203100
0.0250000 0.0306300
0.0500000 0.0462500
0.1000000 0.0675000
0.1500000 0.0827500
0.2000000 0.0970000
0.3000000 0.1175000
0.4000000 0.1250000
0.5000000 0.1135000
0.6000000 0.0970000
0.7000000 0.0775000
0.8000000 0.0550000
0.9000000 0.0285000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0146900
0.0250000 -.0193800
0.0500000 -.0217500
0.1000000 -.0205000
0.1500000 -.0092500
0.2000000 0.0050000
0.3000000 0.0355000
0.4000000 0.0700000
0.5000000 0.0625000
0.6000000 0.0500000
0.7000000 0.0375000
0.8000000 0.0250000
0.9000000 0.0125000
1.0000000 0.0000000
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Polars for SARATOV AIRFOIL (saratov-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| saratov-il | 50,000 | 9 | 18.8 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| saratov-il | 50,000 | 5 | 18.9 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| saratov-il | 100,000 | 9 | 33.7 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| saratov-il | 100,000 | 5 | 48.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| saratov-il | 200,000 | 9 | 161.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| saratov-il | 200,000 | 5 | 77.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| saratov-il | 500,000 | 9 | 112.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| saratov-il | 500,000 | 5 | 113.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| saratov-il | 1,000,000 | 9 | 145.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| saratov-il | 1,000,000 | 5 | 136.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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