Similarly shaped airfoils to GOE 419
New! Bulk download of polars in Excel format: goe419.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. GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
3. NACA M13
4. GOE 590
5. GOE 142 (MVA H.19)
6. GOE 391
7. GOE 377
8. GOE 101
9. GOE 372
10. GOE 393
11. NACA M16
12. GOE 403
13. GOE 235
14. GOE 399
15. NACA45005
16. GOE 100 (SOPWITH)
17. GOE 492
18. GOE 113
19. USA 5
20. GOE 122 (MVA H.2)
21. BE50 (original)