Similarly shaped airfoils to NACA M26
New! Bulk download of polars in Excel format: m26.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.
2. NACA M25 (NACA-TR-221)
3. NACA M25
4. GOE 15
5. GOE 207 (AVIATIK V8)
6. NACA M23 (NACA-TR-221)
7. GOE 300 (FRIEDRICHSHAFEN G20)
8. GOE 14
9. NACA M8
10. GOE 265
11. NACA M23
12. NACA M20
13. NACA M9
14. M 77
15. GOE 198 (L.F.G. 5294)
16. NACA M22 (NACA-TR-221)
17. Horten 9.00% thick 10.00% camber
18. Horten 9.00% thick 9.00% camber
19. NACA M20 (NACA-TR-221)
20. NACA M27
21. GOE 301 (FRIEDRICHSHAFEN G 13)