Similarly shaped airfoils to GOE 323 (HANSA-BRANDENBURG V.1)
New! Bulk download of polars in Excel format: goe323.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
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
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2. GOE 238 (HANSA-BRANDENBURG)
3. EPPLER 598
4. SPICA 11.73% smoothed
5. MILEY M06-13-128
6. NACA63-711 a=0.2
7. NACA6212
8. EPPLER 639
9. FX 77-W-121
10. GOE 167 (V.KARMAN PROP.2)
11. MH 83 13.29%
12. NACA6210
13. NACA64-711 a=0.2
14. GOE 319 (HANSA-BRANDENBURG II)
15. NACA63-710 a=0.2
16. EPPLER 593
17. NACA63-712 a=0.2
18. GOE 591
19. GOE 407
20. GOE 532
21. GOE 385