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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(goe225-il) GOE 225 (MVA H.35) AIRFOIL | Gottingen 225 (MVA H.35) airfoil Max thickness 12.8% at 19.7% chord Max camber 7.6% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(hs1430-il) HAM-STD HS1-430 AIRFOIL | HS1 family of prop airfoils from US Patent No. 4 Max thickness 30% at 34% chord Max camber 3% at 44% chord | Remove Airfoil details Airfoil plotter |
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Polars for (goe225-il,hs1430-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe225-il | 50,000 | 9 | 10.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 50,000 | 5 | 33.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 100,000 | 9 | 59.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 100,000 | 5 | 63.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 200,000 | 9 | 87.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 200,000 | 5 | 83.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 500,000 | 9 | 116.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 500,000 | 5 | 107.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe225-il | 1,000,000 | 9 | 140.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe225-il | 1,000,000 | 5 | 129 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1430-il | 50,000 | 9 | 16.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1430-il | 50,000 | 5 | 14.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1430-il | 100,000 | 9 | 28.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1430-il | 100,000 | 5 | 21.2 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1430-il | 200,000 | 9 | 31 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1430-il | 200,000 | 5 | 22.4 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1430-il | 500,000 | 9 | 27.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1430-il | 500,000 | 5 | 23.6 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1430-il | 1,000,000 | 9 | 29.2 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1430-il | 1,000,000 | 5 | 29.1 at α=12.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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