Similarly shaped airfoils to MARSKE MONARCH (NACA 43012A)


New! Bulk download of polars in Excel format: marske5.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 IID ROOT (NACA 431012A/24112 HYBRID)
2. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
3. NACA34112
4. NACA34113
5. EPPLER 336
6. EPPLER 625
7. NACA33012
8. NACA34013
9. MARSKE XM-1D (F14-3.0)
10. NACA34012
11. Horten 12.00% thick 3.00% camber
12. EPPLER 635
13. NACA44013
14. EPPLER 636
15. NACA44112
16. NACA44113
17. Horten 13.00% thick 4.00% camber
18. NACA33112
19. Horten 12.00% thick 4.00% camber
20. NACA34113.5
21. MH 80 12.72%