Similarly shaped airfoils to NACA64-413 a=0.6
New! Bulk download of polars in Excel format: NACA64-413%20a%3D0.6.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. NACA63-413 a=0.6
3. NACA63-413 a=0.5
4. GA 37-313
5. GA 35-313
6. NACA64-413 a=0.8
7. NACA65-413 a=0.6
8. NACA63-413 a=0.8
9. GA 35A313
10. NACA64-513
11. NACA65-413 a=0.5
12. GA 40-313
13. EPPLER 197
14. GA 40A313
15. NACA63-513
16. GA 37A313
17. PSU-90-125WL
18. NACA64-414 a=0.6
19. NACA64-412 a=0.6
20. NACA63A413
21. NACA65-413 a=0.8