Similarly shaped airfoils to GOE 591


New! Bulk download of polars in Excel format: goe591.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 477
2. GOE 480
3. SPICA 11.73% smoothed
4. GOE 365
5. USA 27
6. GOE 509
7. GOE 321 (HANSA-BRANDENBURG III.1)
8. GOE 574
9. GOE 329 (PFALZ 58)
10. RAF 6
11. GA 30A611
12. GA 30-611
13. NACA63-712 a=0.5
14. NACA63-711 a=0.5
15. NACA64-712 a=0.5
16. NACA64-711 a=0.5
17. GOE 584
18. GOE 532
19. NACA63-712 a=0.6
20. NACA63-711 a=0.6
21. NACA64-712 a=0.6