Similarly shaped airfoils to MARSKE PIONEER IID TIP (NACA 431012A*.833 HYBRID)
New! Bulk download of polars in Excel format: marske4.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
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2. NACA33110
3. NACA42110.5
4. NACA42110
5. NACA33010.5
6. NACA42010.5
7. NACA42010
8. NACA33010
9. NACA32110
10. NACA24110.5
11. NACA32010.5
12. NACA24110
13. NACA32010
14. EMX-07
15. NACA25110.5
16. EPPLER 331
17. EPPLER 635
18. NACA25110
19. Horten 10.00% thick 3.00% camber
20. Horten 11.00% thick 3.00% camber
21. RC_Milan