Similarly shaped airfoils to NACA34109


New! Bulk download of polars in Excel format: NACA34109.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
Dynamic plotter New!
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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1. Horten 9.00% thick 4.00% camber
2. NACA34110
3. NACA34009
4. Horten 10.00% thick 4.00% camber
5. NACA35109
6. Horten 9.00% thick 3.00% camber
7. NACA33109
8. HS 3.0/9.0
9. NACA44109
10. NACA44009
11. Phoenix10
12. NACA34010
13. NACA34110.5
14. NACA35110
15. NACA33009
16. FAD23
17. Horten 10.00% thick 3.00% camber
18. NACA44110
19. NACA33110
20. NACA44010
21. EMX-07