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
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
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2. GOE 15
3. GOE 207 (AVIATIK V8)
4. GOE 300 (FRIEDRICHSHAFEN G20)
5. GOE 14
6. NACA M8
7. GOE 265
8. NACA M23
9. NACA M20
10. NACA M9
11. M 77
12. GOE 198 (L.F.G. 5294)
13. Horten 9.00% thick 10.00% camber
14. Horten 9.00% thick 9.00% camber
15. NACA M27
16. GOE 301 (FRIEDRICHSHAFEN G 13)
17. GOE 311 (MVA H.43)
18. GOE 360
19. GOE 304 (FRIEDRICHSHAFEN G02)
20. Horten 9.00% thick 8.00% camber
21. GOE 364