Similarly shaped airfoils to NACA34112


New! Bulk download of polars in Excel format: NACA34112.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. Horten 12.00% thick 4.00% camber
2. NACA44112
3. EPPLER 636
4. NACA34113
5. NACA34012
6. EPPLER 332
7. Horten 12.00% thick 3.00% camber
8. Horten 13.00% thick 4.00% camber
9. NACA35112
10. EH 3.0/12
11. M-35A-12.7
12. NACA44013
13. NACA44113
14. EPPLER 635
15. Horten 11.00% thick 4.00% camber
16. HS 3.5/12
17. MARSKE MONARCH (NACA 43012A)
18. HS 3.4.12b
19. EPPLER 336
20. NACA44012
21. NACA35012