Similarly shaped airfoils to GOE 287
New! Bulk download of polars in Excel format: goe287.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 277 (DAIMLER VIII)
3. GOE 308 (MVA H.40)
4. GOE 314 (HANSA-BRANDENBURG)
5. GOE 188
6. GOE 325 (PFALZ 54)
7. WACO COOTIE
8. NACA63-709 a=0.2
9. GOE 281 (DAIMLER XII)
10. GOE 180 (MVA H.26)
11. GOE 328
12. NACA64-709 a=0.2
13. GOE 280 (DAIMLER XI)
14. USA 22
15. GOE 238 (HANSA-BRANDENBURG)
16. GOE 167 (V.KARMAN PROP.2)
17. GOE 140 (MVA H.17)
18. GOE 336 (MVA H.44)
19. NACA63-709 a=0.5
20. S4320
21. GOE 310 (MVA H.42)