Similarly shaped airfoils to NACA33110.5
New! Bulk download of polars in Excel format: NACA33110.5.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. NACA33010.5
3. MARSKE PIONEER IID TIP (NACA 431012A*.833 HYBRID)
4. NACA33010
5. NACA42010.5
6. NACA42110.5
7. NACA42010
8. NACA24110.5
9. NACA25110.5
10. EPPLER 331
11. NACA42110
12. Horten 11.00% thick 3.00% camber
13. NACA24110
14. EPPLER 635
15. NACA25110
16. Horten 10.00% thick 3.00% camber
17. NACA32010.5
18. EMX-07
19. NACA32110
20. NACA34110.5
21. NACA34010.5