Similarly shaped airfoils to GOE 324 (HANSA-BRANDENBURG)


New! Bulk download of polars in Excel format: goe324.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 322 (HANSA-BRANDENBURG IV.1)
2. FX 049-915
3. NACA6212
4. NACA M21 (NACA-TR-221)
5. NACA M21
6. NACA M24 (NACA-TR-221)
7. GOE 321 (HANSA-BRANDENBURG III.1)
8. GOE 404
9. GOE 530
10. GOE 320 (HANSA-BRANDENBURG II.1)
11. GOE 654
12. GOE 365
13. NACA M24
14. GOE 406
15. MH 83 13.29%
16. GOE 769
17. GOE 323 (HANSA-BRANDENBURG V.1)
18. GOE 319 (HANSA-BRANDENBURG II)
19. GOE 418
20. GOE 615
21. GOE 744