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
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. 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%