Similarly shaped airfoils to MARSKE XM-1D (F14-3.0)
New! Bulk download of polars in Excel format: marske1.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. FAUVEL 14%
3. LA2573A
4. Horten 13.00% thick 4.00% camber
5. Horten 13.00% thick 3.00% camber
6. NACA34113
7. NACA34113.5
8. MARSKE MONARCH (NACA 43012A)
9. Horten 14.00% thick 4.00% camber
10. MH 80 12.72%
11. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
12. EPPLER 625
13. EPPLER 336
14. Horten 14.00% thick 3.00% camber
15. HG 42
16. NACA34114
17. NACA25113
18. MARSKE PIONEER IA (NACA 23112/43012A HYBRID)
19. NACA25113.5
20. Horten 12.00% thick 3.00% camber
21. EPPLER 341