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
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.
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