Similarly shaped airfoils to NACA44110


New! Bulk download of polars in Excel format: NACA44110.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. NACA44110.5
2. NACA35110
3. Horten 10.00% thick 5.00% camber
4. NACA44109
5. NACA35110.5
6. NACA34110
7. NACA44010
8. Horten 11.00% thick 5.00% camber
9. NACA35109
10. Horten 10.00% thick 4.00% camber
11. NACA44010.5
12. NACA34110.5
13. NACA45110
14. Horten 9.00% thick 5.00% camber
15. Horten 9.00% thick 4.00% camber
16. NACA45110.5
17. NACA34109
18. NACA44009
19. Horten 11.00% thick 4.00% camber
20. NACA45010
21. NACA45010.5