Similarly shaped airfoils to GOE 410
New! Bulk download of polars in Excel format: goe410.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
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.
2. EPPLER 479
3. EPPLER 478
4. SU-26M
5. Joukowsky 17.00% thick 0.00% camber
6. EPPLER 473
7. Joukowsky 15.00% thick 0.00% camber
8. Horten 15.00% thick 0.00% camber
9. EPPLER 475
10. FX 71-L-150/30
11. EPPLER 477
12. Horten 16.00% thick 0.00% camber
13. FX 71-L-150/25
14. FX 71-L-150/20
15. GA 30-015
16. NACA0015
17. GA 35-016
18. Joukowsky 18.00% thick 0.00% camber
19. Horten 15.00% thick 1.00% camber
20. GA 35-015
21. NACA63-015