Similarly shaped airfoils to GOE 286
New! Bulk download of polars in Excel format: goe286.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 316 (HANSA-BRANDENBURG IV.5)
3. GOE 596
4. GOE 385
5. GOE 490
6. GOE 257
7. GOE 318 (HANSA-BRANDENBURG VI.5)
8. GOE 167 (V.KARMAN PROP.2)
9. FAD21
10. GOE 134 (MVA H.12)
11. USA 22
12. GOE 277 (DAIMLER VIII)
13. GOE 188
14. GOE 389
15. NACA63-710 a=0.2
16. USA 26
17. GOE 309 (MVA H.41)
18. NACA63-710 a=0.0
19. NACA63-709 a=0.0
20. NACA63-709 a=0.2
21. GOE 180 (MVA H.26)