Similarly shaped airfoils to NACA63A618
New! Bulk download of polars in Excel format: NACA63A618.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
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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2. NACA65-618 a=0.8
3. NACA63A619
4. NACA63A617
5. NACA64A619
6. NACA65-718
7. NACA64-618 a=0.8
8. NACA64-619 a=0.8
9. NACA64A617
10. NACA64-718
11. NACA64-719
12. NACA65-619 a=0.8
13. HQ 3.5/18
14. NACA63A718
15. NACA63A518
16. NACA64A518
17. NACA65-719
18. NACA64(3)-618
19. GA 35A418
20. NACA63-618 a=0.8
21. NACA65A618