Similarly shaped airfoils to NACA65-714
New! Bulk download of polars in Excel format: NACA65-714.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (6) | 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. NACA64A614
3. NACA64-714
4. NACA63A614
5. NACA65A614
6. NACA64-614 a=0.8
7. NACA65-715
8. NACA65-713
9. FX 75-141
10. NACA65-514 a=0.8
11. NACA65-614
12. NACA65A613
13. NACA65-615 a=0.8
14. NACA64A613
15. NACA64-715
16. NACA65-613 a=0.8
17. NACA63A613
18. NACA63-714
19. NACA64-615 a=0.8
20. EPPLER 68
21. EPPLER 668