Similarly shaped airfoils to GOE 207 (AVIATIK V8)


New! Bulk download of polars in Excel format: goe207.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 300 (FRIEDRICHSHAFEN G20)
2. GOE 360
3. NACA6209
4. GOE 173 (ALBATROS 6020)
5. GOE 14
6. GOE 359
7. GOE 311 (MVA H.43)
8. NACA M23 (NACA-TR-221)
9. GOE 174 (ALBATROS 5020)
10. NACA M20
11. GOE 304 (FRIEDRICHSHAFEN G02)
12. GOE 529
13. GOE 140 (MVA H.17)
14. GOE 198 (L.F.G. 5294)
15. NACA6210
16. GOE 301 (FRIEDRICHSHAFEN G 13)
17. GOE 801 (MVA 301)
18. GOE 802
19. GOE 124 (MVA H.4)
20. GOE 319 (HANSA-BRANDENBURG II)
21. NACA M9