Similarly shaped airfoils to NACA65A515
New! Bulk download of polars in Excel format: NACA65A515.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (8) | 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. NACA66A515
3. NACA66-515 a=0.8
4. NACA66-615
5. NACA65-515 a=0.8
6. NACA65-615
7. NACA65A516
8. NACA65A514
9. NACA65-516 a=0.8
10. NACA64A516
11. NACA63A515
12. NACA66A514
13. NACA65-616
14. NACA66-514 a=0.8
15. NACA66-614
16. AH 82-150 A
17. NACA66-515 a=0.6
18. NACA65-515 a=0.6
19. NACA65A415
20. NACA65A615
21. GA 37A415