Similarly shaped airfoils to GOE 646


New! Bulk download of polars in Excel format: goe646.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 420
2. EPPLER 856
3. Joukowsky 19.00% thick 5.00% camber
4. GOE 255 (MVA CA.6)
5. EPPLER 748
6. GOE 679
7. Joukowsky 18.00% thick 5.00% camber
8. Joukowsky 20.00% thick 5.00% camber
9. GA 30-618
10. GA 30U-618
11. NACA63-719 a=0.8
12. GOE 433
13. NACA63-718 a=0.8
14. GA 30A618
15. GA 30-617
16. SB99A22CO
17. GOE 681
18. GA 30A617
19. NACA63A718
20. FX 84-W-175
21. Joukowsky 19.00% thick 4.00% camber