Similarly shaped airfoils to NACA25115
New! Bulk download of polars in Excel format: NACA25115.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. Horten 15.00% thick 3.00% camber
3. Horten 15.00% thick 2.00% camber
4. NACA24115
5. NACA33015
6. NACA24114.5
7. NACA33014.5
8. NACA34015
9. NACA25116
10. NACA25114
11. NACA24015
12. NACA33115
13. Horten 16.00% thick 3.00% camber
14. NACA24014.5
15. Horten 16.00% thick 2.00% camber
16. NACA25015
17. NACA33114.5
18. NACA24114
19. NACA33014
20. NACA33016
21. Horten 14.00% thick 2.00% camber