Similarly shaped airfoils to NACA65A615
New! Bulk download of polars in Excel format: NACA65A615.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. NACA66A615
3. NACA66-615 a=0.8
4. NACA65-615 a=0.8
5. NACA66-715
6. NACA65-715
7. NACA65A616
8. NACA65A614
9. NACA65-616 a=0.8
10. NACA64A616
11. NACA63A615
12. NACA66A614
13. NACA66-614 a=0.8
14. NACA65-716
15. NACA66-714
16. NACA65A515
17. NACA65A715
18. AH 82-150 A
19. NACA66-615 a=0.6
20. NACA63A616
21. NACA65-615 a=0.6