Similarly shaped airfoils to NACA34119


New! Bulk download of polars in Excel format: NACA34119.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. NACA44019
2. NACA44119
3. Horten 19.00% thick 4.00% camber
4. NACA34118
5. NACA34019
6. Horten 19.00% thick 3.00% camber
7. NACA35119
8. Horten 20.00% thick 4.00% camber
9. NACA44118
10. Horten 18.00% thick 4.00% camber
11. NACA35019
12. Horten 20.00% thick 3.00% camber
13. NACA25119
14. NACA34018
15. Horten 18.00% thick 3.00% camber
16. NACA35118
17. Horten 20.00% thick 5.00% camber
18. NACA45119
19. NACA25118
20. NACA35018
21. NACA33018