Similarly shaped airfoils to NACA M26 (NACA-TR-221)


New! Bulk download of polars in Excel format: NACA%20M26%20%28NACA-TR-221%29.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.

1. NACA M26
2. NACA M25 (NACA-TR-221)
3. NACA M25
4. GOE 15
5. GOE 207 (AVIATIK V8)
6. GOE 300 (FRIEDRICHSHAFEN G20)
7. NACA M23 (NACA-TR-221)
8. GOE 14
9. NACA M8
10. GOE 265
11. NACA M9
12. NACA M23
13. M 77
14. NACA M20
15. GOE 198 (L.F.G. 5294)
16. GOE 301 (FRIEDRICHSHAFEN G 13)
17. NACA M22 (NACA-TR-221)
18. GOE 304 (FRIEDRICHSHAFEN G02)
19. NACA M27
20. NACA M20 (NACA-TR-221)
21. Horten 9.00% thick 10.00% camber