Similarly shaped airfoils to GOE 315 (HANSA-BRANDENBURG III.5)


New! Bulk download of polars in Excel format: goe315.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

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1. GOE 122 (MVA H.2)
2. GOE 415
3. GOE 316 (HANSA-BRANDENBURG IV.5)
4. NACA63-709 a=0.0
5. GOE 143 (MVA H.20)
6. GOE 318 (HANSA-BRANDENBURG VI.5)
7. NACA64-709 a=0.0
8. NACA M14
9. NACA63-609 a=0.2
10. GOE 314 (HANSA-BRANDENBURG)
11. GOE 133 (MVA H.11)
12. NACA63-709 a=0.2
13. GOE 277 (DAIMLER VIII)
14. NACA64-609 a=0.2
15. USA 22
16. GOE 278 (DAIMLER IX)
17. NACA M17 (NACA-TR-221)
18. NACA64-709 a=0.2
19. GOE 328
20. GOE 276 (DAIMLER VII)
21. AQUILA 9.3% smoothed