Similarly shaped airfoils to MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)


New! Bulk download of polars in Excel format: marske3.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
Dynamic plotter New!
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.

1. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
2. MARSKE MONARCH (NACA 43012A)
3. NACA33012
4. NACA33112
5. EPPLER 336
6. NACA42012
7. Horten 12.00% thick 3.00% camber
8. NACA42112
9. NACA25112
10. EPPLER 635
11. EPPLER 327
12. NACA25113
13. NACA33113
14. EPPLER 331
15. NACA33013
16. NACA42013
17. EPPLER 625
18. Horten 13.00% thick 3.00% camber
19. NACA34112
20. NACA42113
21. NACA34012