Airfoil Comparison
Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
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(tsagi8-il) TSAGI 8% AIRFOIL | TSAGI 8% airfoil Max thickness 8% at 30% chord Max camber 1.3% at 30% chord | Remove Airfoil details Airfoil plotter |
(tsagi-r-3a-il) TsAGI R-3a (12%) | TsAGI R-3a used on Russian ultra light aircraft (12%). Max thickness 12.1% at 23.1% chord Max camber 3.1% at 24.1% chord | Remove Airfoil details Airfoil plotter |
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Polars for (tsagi8-il,tsagi-r-3a-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| tsagi8-il | 50,000 | 9 | 32.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 50,000 | 5 | 32.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 100,000 | 9 | 45.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 100,000 | 5 | 44.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 200,000 | 9 | 57.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 200,000 | 5 | 55.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 500,000 | 9 | 72.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 500,000 | 5 | 65.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi8-il | 1,000,000 | 9 | 76.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi8-il | 1,000,000 | 5 | 69.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 50,000 | 9 | 16.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 50,000 | 5 | 25.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 100,000 | 9 | 33 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 100,000 | 5 | 43.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 200,000 | 9 | 56.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 200,000 | 5 | 60.8 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 500,000 | 9 | 86.5 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 500,000 | 5 | 88.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 1,000,000 | 9 | 112.1 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tsagi-r-3a-il | 1,000,000 | 5 | 108.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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