Similarly shaped airfoils to NACA64-613
New! Bulk download of polars in Excel format: NACA64-613.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. NACA64-513 a=0.8
3. NACA63-513 a=0.8
4. NACA63A513
5. NACA65-613
6. HQ 3.0/13
7. NACA65-513 a=0.8
8. NACA64A513
9. EPPLER 854
10. NACA63A512
11. NACA64-614
12. NACA64-612
13. EM J18 3013
14. SB 96 12.7/3.0
15. NACA63-612
16. NACA64-512 a=0.8
17. NACA64-514 a=0.8
18. NACA63-614
19. NACA64A512
20. HQ 3.0/12
21. NACA64-513 a=0.6