Similarly shaped airfoils to GOE 321 (HANSA-BRANDENBURG III.1)


New! Bulk download of polars in Excel format: goe321.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. SPICA 11.73% smoothed
2. GOE 323 (HANSA-BRANDENBURG V.1)
3. NACA6212
4. GOE 509
5. GOE 591
6. GOE 365
7. USA 27
8. GOE 319 (HANSA-BRANDENBURG II)
9. EPPLER 639
10. NACA6210
11. GOE 407
12. GOE 532
13. GOE 238 (HANSA-BRANDENBURG)
14. GOE 477
15. GOE 329 (PFALZ 58)
16. NACA M9 (NACA-TR-221)
17. GOE 574
18. GOE 584
19. GA 30-611
20. RAF 6
21. GOE 167 (V.KARMAN PROP.2)