Similarly shaped airfoils to NACA64A716
New! Bulk download of polars in Excel format: NACA64A716.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. NACA65-716 a=0.8
3. NACA65A716
4. NACA64A717
5. NACA64A715
6. NACA63A715
7. NACA64-716 a=0.8
8. NACA65-717 a=0.8
9. NACA63A717
10. NACA65A715
11. NACA64-717 a=0.8
12. NACA65-616 a=0.8
13. NACA65-715 a=0.8
14. NACA64A616
15. NACA63A616
16. NACA63-716 a=0.8
17. EPPLER 431
18. EPPLER 662
19. NACA65-716 a=0.6
20. GA 37A616
21. EPPLER 657