Similarly shaped airfoils to GOE 164 (MVA MK.10)


New! Bulk download of polars in Excel format: goe164.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 198 (L.F.G. 5294)
2. SOKOLOV
3. MID 115-7
4. GOE 304 (FRIEDRICHSHAFEN G02)
5. Joukowsky 9.00% thick 7.00% camber
6. GOE 610-B MOD.
7. GOE 173 (ALBATROS 6020)
8. GOE 359
9. M 7372
10. GOE 265
11. GOE 300 (FRIEDRICHSHAFEN G20)
12. M 77
13. Joukowsky 9.00% thick 6.00% camber
14. MID 112
15. NACA6409
16. Joukowsky 10.00% thick 7.00% camber
17. MID 114
18. AH-6-40-7
19. EPPLER 385
20. GOE 395
21. GOE 500