Similarly shaped airfoils to GOE 509


New! Bulk download of polars in Excel format: goe509.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. USA 27
2. GOE 365
3. GOE 591
4. GOE 321 (HANSA-BRANDENBURG III.1)
5. GOE 406
6. SPICA 11.73% smoothed
7. NACA6212
8. RAF 6
9. NACA M9 (NACA-TR-221)
10. GOE 574
11. USNPS4 (smoothed)
12. NACA M21 (NACA-TR-221)
13. NACA M21
14. GOE 584
15. GOE 530
16. GOE 407
17. GOE 480
18. GOE 477
19. GA 30A612
20. CURTIS CR-1
21. GOE 329 (PFALZ 58)