Similarly shaped airfoils to NACA44119


New! Bulk download of polars in Excel format: NACA44119.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. NACA34119
2. NACA44118
3. Horten 19.00% thick 4.00% camber
4. NACA35119
5. NACA34118
6. NACA44019
7. Horten 20.00% thick 5.00% camber
8. Horten 20.00% thick 4.00% camber
9. NACA45119
10. Horten 18.00% thick 4.00% camber
11. NACA35118
12. Horten 19.00% thick 3.00% camber
13. NACA34019
14. Horten 19.00% thick 5.00% camber
15. Horten 20.00% thick 3.00% camber
16. NACA44121
17. NACA44117
18. NACA35019
19. NACA34018
20. NACA25119
21. Horten 18.00% thick 3.00% camber