Similarly shaped airfoils to GOE 15


New! Bulk download of polars in Excel format: goe15.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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. GOE 14
2. GOE 300 (FRIEDRICHSHAFEN G20)
3. GOE 331 (PFALZ 60)
4. GOE 301 (FRIEDRICHSHAFEN G 13)
5. NACA M26 (NACA-TR-221)
6. NACA M26
7. GOE 364
8. GOE 207 (AVIATIK V8)
9. GOE 304 (FRIEDRICHSHAFEN G02)
10. GOE 198 (L.F.G. 5294)
11. GOE 801 (MVA 301)
12. GOE 802
13. GOE 265
14. NACA M8
15. M 77
16. NACA M27 (NACA-TR-221)
17. GOE 630
18. GOE 360
19. GOE 405
20. DAE-31
21. GOE 164 (MVA MK.10)