Similarly shaped airfoils to NACA63A714
New! Bulk download of polars in Excel format: NACA63A714.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. NACA64-714 a=0.8
3. NACA65-714 a=0.8
4. NACA64-715 a=0.8
5. NACA63-714 a=0.8
6. NACA63A715
7. NACA63A713
8. NACA64A715
9. NACA65A714
10. NACA64A713
11. NACA63-715 a=0.8
12. EPPLER 668
13. NACA65-715 a=0.8
14. NACA65A713
15. NACA65-614 a=0.8
16. FX 84-W-140
17. NACA63A614
18. NACA64A614
19. MID 403
20. NACA65-713 a=0.8
21. NACA64-614 a=0.8