Similarly shaped airfoils to NACA63A513
New! Bulk download of polars in Excel format: NACA63A513.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. NACA65-513 a=0.8
4. NACA64-613
5. NACA65-613
6. NACA63-513 a=0.8
7. NACA64-514 a=0.8
8. EPPLER 68
9. NACA63-613
10. NACA65A513
11. NACA64-614
12. HQ 3.0/13
13. CB3013
14. NACA63A514
15. NACA63A512
16. NACA64A514
17. GA 35A413
18. NACA64A512
19. GA 37A413
20. NACA63-514 a=0.8
21. EPPLER 854