Similarly shaped airfoils to GOE 426
New! Bulk download of polars in Excel format: goe426.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (5) | 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 549
3. GA 35-614
4. GA 35-613
5. GOE 584
6. GA 30-613
7. GOE 533
8. USA 40
9. SD7062 (14%)
10. GOE 553
11. NACA63-713 a=0.5
12. NACA63-713 a=0.6
13. EPPLER 210
14. GA 30A613
15. GA 37-613
16. GA 37-614
17. NACA63-714 a=0.5
18. NACA63-714 a=0.6
19. GOE 655
20. GA 35A613
21. GOE 619