Similarly shaped airfoils to NACA65A619


New! Bulk download of polars in Excel format: NACA65A619.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. NACA65A620
2. NACA65A618
3. NACA64A619
4. NACA66-619 a=0.8
5. NACA66A619
6. NACA66-719
7. NACA65-619 a=0.8
8. NACA64A620
9. NACA66-618 a=0.8
10. NACA66A618
11. NACA65-620 a=0.8
12. NACA65A519
13. NACA65-719
14. NACA65A719
15. NACA66-718
16. NACA65-720
17. NACA63A619
18. NACA66-619 a=0.6
19. NACA64A719
20. NACA66A719
21. NACA64A618