Similarly shaped airfoils to GOE 590


New! Bulk download of polars in Excel format: goe590.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. NACA M16 (NACA-TR-221)
2. NACA M16
3. NACA M13 (NACA-TR-221)
4. NACA M13
5. GOE 419
6. NACA M7 (NACA-TR-221)
7. GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
8. NACA45005
9. GOE 397
10. GOE 393
11. GOE 142 (MVA H.19)
12. NACA35005
13. GOE 377
14. GOE 391
15. GOE 235
16. NACA45007
17. GOE 101
18. GOE 113
19. GOE 587
20. NACA35007
21. NACA44005