Similarly shaped airfoils to NACA44112


New! Bulk download of polars in Excel format: NACA44112.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. NACA34112
2. NACA44113
3. Horten 12.00% thick 4.00% camber
4. NACA35112
5. NACA34113
6. Horten 13.00% thick 4.00% camber
7. NACA35113
8. EPPLER 636
9. Horten 11.00% thick 4.00% camber
10. M-35A-12.7
11. Horten 12.00% thick 5.00% camber
12. NACA44113.5
13. HS 3.5/12
14. NACA44013
15. NACA44012
16. NACA45113
17. NACA34110.5
18. Horten 13.00% thick 5.00% camber
19. HS 3.4.12b
20. EPPLER 332
21. EPPLER 637