Similarly shaped airfoils to NACA64A720
New! Bulk download of polars in Excel format: NACA64A720.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. NACA65-720 a=0.8
3. NACA64A719
4. NACA63A719
5. NACA65A720
6. NACA65A719
7. NACA64A620
8. NACA64-720 a=0.8
9. NACA65-719 a=0.8
10. NACA63A620
11. NACA65-620 a=0.8
12. GA 37A620
13. NACA65-720 a=0.6
14. NACA65A620
15. GA 35A620
16. NACA64A619
17. NACA65A619
18. NACA65-620 a=0.6
19. GA 40A620
20. NACA63A619
21. GA 40-620