Similarly shaped airfoils to NACA64-618
New! Bulk download of polars in Excel format: NACA64-618.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (54) | 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. NACA63-618
3. NACA63-518 a=0.8
4. NACA64-619
5. NACA64-617
6. NACA64-517 a=0.8
7. NACA64-519 a=0.8
8. NACA64-518
9. NACA64-518 a=0.6
10. NACA64-718
11. NACA63A517
12. NACA63(420)-517
13. NACA63A518
14. NACA63-617
15. NACA63-619
16. NACA65-618
17. NACA63-518
18. NACA64(3)-418
19. NACA63-517 a=0.8
20. NACA63-519 a=0.8
21. NACA65-518 a=0.8