Similarly shaped airfoils to GOE 322 (HANSA-BRANDENBURG IV.1)


New! Bulk download of polars in Excel format: goe322.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 320 (HANSA-BRANDENBURG II.1)
2. GOE 562
3. GOE 573
4. GOE 611
5. GOE 615
6. GOE 324 (HANSA-BRANDENBURG)
7. GOE 406
8. GOE 528
9. NACA M24 (NACA-TR-221)
10. GOE 654
11. GOE 365
12. NACA M21
13. NACA M21 (NACA-TR-221)
14. GOE 530
15. FX 049-915
16. Glenn Martin 2
17. GOE 387
18. GOE 332 (PFALZ 61)
19. GOE 404
20. GOE 398
21. GOE 512