Similarly shaped airfoils to EPPLER 336
New! Bulk download of polars in Excel format: e336.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. EPPLER 625
3. NACA25113
4. EPPLER 341
5. NACA34113
6. Horten 13.00% thick 3.00% camber
7. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
8. NACA25113.5
9. Horten 12.00% thick 3.00% camber
10. NACA34113.5
11. NACA34013
12. EPPLER 340
13. NACA25112
14. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
15. Horten 13.00% thick 4.00% camber
16. EPPLER 335
17. NACA34112
18. NACA34013.5
19. NACA33012
20. NACA44013
21. CLARK YS