Similarly shaped airfoils to GOE 425
New! Bulk download of polars in Excel format: goe425.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. GA 30-615
3. GA 30U-615
4. NACA63-716 a=0.5
5. GA 30A615
6. GA 37-616
7. GA 35A616
8. GA 30-616
9. NACA64-716 a=0.5
10. GA 35-617
11. NACA63-716 a=0.6
12. GA 35A615
13. GA 30A616
14. GA 35-615
15. GOE 648
16. FX 66-17A-175
17. NACA63-715 a=0.5
18. NACA63-717 a=0.5
19. NACA64-716 a=0.6
20. GA 37-617
21. FX 84-W-150