Similarly shaped airfoils to NACA65A715
New! Bulk download of polars in Excel format: NACA65A715.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. NACA66A715
3. NACA66-715 a=0.8
4. NACA65-715 a=0.8
5. NACA65A716
6. NACA65A714
7. NACA65-716 a=0.8
8. NACA64A716
9. NACA63A715
10. EPPLER 662
11. NACA66A714
12. NACA66-714 a=0.8
13. HQ-17
14. EPPLER 433
15. EPPLER 668
16. NACA65A615
17. EPPLER 431
18. NACA63A716
19. NACA64A714
20. EPPLER STE 87(-3)-914
21. NLF-1015