Similarly shaped airfoils to GOE 549
New! Bulk download of polars in Excel format: goe549.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (47) | 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 426
3. GOE 655
4. GOE 584
5. GA 30-613
6. GA 35-614
7. SD7062 (14%)
8. GOE 533
9. GA 30A613
10. NACA63-714 a=0.5
11. GOE 398
12. GOE 553
13. GOE 619
14. NACA63-714 a=0.6
15. GOE 478
16. GA 37-614
17. GA 30-614
18. GOE 701
19. NACA64-714 a=0.5
20. GA 35A614
21. GOE 404