Similarly shaped airfoils to EPPLER 335
New! Bulk download of polars in Excel format: e335.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA33113
3. NACA33112
4. EPPLER 340
5. EPPLER 325
6. NACA24113
7. NACA42113
8. NACA24112
9. NACA33113.5
10. NACA42112
11. Horten 13.00% thick 3.00% camber
12. EPPLER 336
13. NACA33013
14. NACA42013
15. NACA24113.5
16. EPPLER 327
17. NACA32113
18. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
19. NACA32112
20. NACA42012
21. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)