Similarly shaped airfoils to NACA33112
New! Bulk download of polars in Excel format: NACA33112.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
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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2. NACA42012
3. NACA24112
4. NACA33113
5. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
6. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
7. NACA42113
8. NACA32112
9. NACA33013
10. EPPLER 335
11. NACA33012
12. NACA42013
13. NACA32012
14. NACA25112
15. Horten 12.00% thick 2.00% camber
16. EPPLER 635
17. Horten 13.00% thick 3.00% camber
18. NACA24113
19. NACA33113.5
20. EPPLER 326
21. NACA24012