Similarly shaped airfoils to GOE 460


New! Bulk download of polars in Excel format: goe460.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

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1. NACA0021
2. GA 30A020
3. GA 30-020
4. GOE 775
5. Horten 20.00% thick 0.00% camber
6. GA 35A020
7. GA 37A020
8. Horten 20.00% thick 1.00% camber
9. GA 30A019
10. GA 30-019
11. NACA63A120
12. NACA65-021
13. NACA64-021
14. NACA64A120
15. NACA23021
16. NACA24021
17. Horten 19.00% thick 0.00% camber
18. NACA63-021
19. NACA2221
20. GA 40A020
21. NACA22021