Similarly shaped airfoils to NACA65-009
New! Bulk download of polars in Excel format: NACA65-009.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. LWK 80-080
3. NACA63-009
4. MH 52
5. Dale House DH4009 (smoothed) used on the Storm R/C aerobatic aircraft
6. NACA66-009
7. MH 50
8. GA 40-010
9. GA 40A010
10. NACA M2
11. GA 37-010
12. NACA0008-34
13. EH 0.0/9.0
14. GA 37A010
15. NACA65-109 a=0.0
16. NACA0009
17. NACA65-109
18. EPPLER EA 6(-1)-009
19. NACA64A-010
20. Horten 9.00% thick 0.00% camber
21. GA 35A010