Similarly shaped airfoils to GOE 574
New! Bulk download of polars in Excel format: goe574.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 477
3. RAF 6
4. GOE 591
5. GOE 167 (V.KARMAN PROP.2)
6. GOE 282 (DAIMLER XIII)
7. GOE 329 (PFALZ 58)
8. GOE 392
9. GA 30A610
10. NACA65-710 a=0.5
11. GOE 613
12. Fage & Collins 3
13. GA 37A611
14. NACA65-711 a=0.5
15. GA 35A611
16. NACA66-710 a=0.5
17. GA 37A610
18. GA 35A610
19. GOE 336 (MVA H.44)
20. GA 30-610
21. GOE 134 (MVA H.12)