Similarly shaped airfoils to NACA34019


New! Bulk download of polars in Excel format: NACA34019.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. NACA35019
3. Horten 19.00% thick 3.00% camber
4. NACA25119
5. NACA34018
6. NACA34119
7. Horten 20.00% thick 3.00% camber
8. NACA25118
9. NACA33018
10. NACA35018
11. Horten 18.00% thick 3.00% camber
12. NACA24119
13. Horten 19.00% thick 4.00% camber
14. NACA25019
15. NACA34118
16. NACA24019
17. NACA2219
18. NACA24118
19. Horten 18.00% thick 2.00% camber
20. Horten 20.00% thick 4.00% camber
21. NACA25018