Similarly shaped airfoils to EPPLER 635
New! Bulk download of polars in Excel format: e635.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. Horten 11.00% thick 3.00% camber
3. Horten 12.00% thick 3.00% camber
4. EPPLER 636
5. EH 3.0/12
6. NACA33110.5
7. NACA34112
8. NACA25112
9. EPPLER 332
10. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
11. NACA25110.5
12. NACA33112
13. NACA33012
14. Horten 11.00% thick 4.00% camber
15. Horten 12.00% thick 4.00% camber
16. NACA34110.5
17. CLARK YS
18. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
19. MARSKE PIONEER IID TIP (NACA 431012A*.833 HYBRID)
20. NACA33010.5
21. NACA24110.5