Similarly shaped airfoils to GA 35A619


New! Bulk download of polars in Excel format: GA%2035A619.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord

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1. GA 37A619
2. GA 40A619
3. GA 35A618
4. GA 35A620
5. GA 40-619
6. GA 37-619
7. GA 37-620
8. GA 37A620
9. GA 37A618
10. NACA65-719 a=0.5
11. NACA65-719 a=0.6
12. GA 30-618
13. GA 30U-618
14. GA 40A620
15. GA 30-619
16. GA 35-619
17. GA 40-620
18. GA 30A618
19. GA 35-620
20. NACA64-719 a=0.6
21. NACA64-719 a=0.5