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
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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
1. GOE 407
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)