Similarly shaped airfoils to NACA64A715
New! Bulk download of polars in Excel format: NACA64A715.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. NACA65-715 a=0.8
3. NACA65A715
4. NACA64-715 a=0.8
5. NACA64A716
6. NACA64A714
7. NACA63A714
8. NACA65-716 a=0.8
9. NACA65A714
10. NACA63A716
11. EPPLER 668
12. NACA64-716 a=0.8
13. EPPLER 433
14. NACA65-615 a=0.8
15. NACA65-714 a=0.8
16. NACA63-715 a=0.8
17. NACA64A615
18. EPPLER 431
19. NACA63A615
20. NACA65-715 a=0.6
21. GA 37A615