Similarly shaped airfoils to NACA63A718
New! Bulk download of polars in Excel format: NACA63A718.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. NACA65-718 a=0.8
3. NACA63A719
4. NACA63A717
5. NACA64A719
6. NACA64-718 a=0.8
7. NACA64-719 a=0.8
8. NACA64A717
9. FX 84-W-175
10. NACA65-719 a=0.8
11. NACA63A618
12. NACA64A618
13. NACA63-718 a=0.8
14. NACA65A718
15. NACA63-719 a=0.8
16. EPPLER 655
17. NACA65-618 a=0.8
18. GA 35A618
19. HQ 3.5/18
20. GA 37A618
21. NACA65A717