Similarly shaped airfoils to NACA64A515
New! Bulk download of polars in Excel format: NACA64A515.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (10) | 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. NACA65-515 a=0.8
3. NACA65-615
4. NACA65A515
5. NACA64-515 a=0.8
6. NACA64A516
7. NACA64A514
8. NACA64-615
9. NACA63A514
10. GA 37A415
11. NACA65-516 a=0.8
12. USA 48
13. GOE 493
14. NACA65A514
15. NACA65-515 a=0.6
16. NACA63A516
17. NACA65-616
18. NACA64-516 a=0.8
19. GA 35A415
20. NACA64-616
21. NACA65(2)-415 a=0.5