Similarly shaped airfoils to GOE 546


New! Bulk download of polars in Excel format: goe546.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 602
2. SG6042
3. NACA4410
4. MID 321c
5. HQ 3.5/10
6. EPPLER E193gU-K24
7. RAF 32 MOD
8. NACA63-711
9. MS3,3-11GP
10. K3311 (original)
11. S7055 (10.5%) Flat-Bottomed
12. SB96 10.5/3.0
13. K3311 (smoothed)
14. NACA63A610
15. SG6041_PSO
16. NACA64-711
17. GOE 547
18. JWL041 11/3.5
19. GOE 602 MOD.
20. NACA63-611 a=0.8
21. NACA63A611