Similarly shaped airfoils to NACA42012
New! Bulk download of polars in Excel format: NACA42012.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA33112
3. NACA32012
4. NACA24112
5. NACA42013
6. NACA32112
7. NACA33012
8. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
9. NACA24012
10. NACA33013
11. Horten 12.00% thick 2.00% camber
12. NACA42113
13. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
14. NACA33113
15. NACA25112
16. EPPLER 361
17. NACA23112
18. EH 2.0/12
19. NACA 2R212
20. NACA25012
21. NACA32013