Similarly shaped airfoils to GOE 550
New! Bulk download of polars in Excel format: goe550.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. GOE 650
3. Joukowsky 13.00% thick 4.00% camber
4. NM Retro 13
5. GS-1
6. MS535-2
7. NM Retro 14
8. Joukowsky 14.00% thick 4.00% camber
9. USA 40
10. FX 60-126/1
11. WB-135/35 13.5% smoothed
12. GOE 619
13. EPPLER 210
14. GOE 298
15. Joukowsky 12.00% thick 4.00% camber
16. NACA4412
17. GOE 430
18. Joukowsky 13.00% thick 5.00% camber
19. GOE 723
20. GA 30-612
21. GA 30U-612