Similarly shaped airfoils to NACA63A613


Direct link: NACA63A613
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
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. NACA64A613
2. NACA64-613 a=0.8
3. NACA65-613 a=0.8
4. NACA65-713
5. NACA64-713
6. NACA63-613 a=0.8
7. NACA64-614 a=0.8
8. EPPLER 68
9. NACA65A613
10. NACA63-713
11. NACA63A614
12. NACA63A612
13. NACA64-714
14. NACA64A614
15. HQ 3.5/13
16. NACA64A612
17. NACA63-614 a=0.8
18. NACA65-614 a=0.8
19. NACA63-714
20. NACA65-714
21. EPPLER 854