Similarly shaped airfoils to SU-26M


New! Bulk download of polars in Excel format: SU-26M.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. EPPLER 479
2. GOE 410
3. Joukowsky 16.00% thick 0.00% camber
4. EPPLER 478
5. EPPLER 473
6. Joukowsky 17.00% thick 0.00% camber
7. Joukowsky 15.00% thick 0.00% camber
8. Joukowsky 18.00% thick 0.00% camber
9. EPPLER 475
10. Horten 15.00% thick 0.00% camber
11. Horten 16.00% thick 0.00% camber
12. EPPLER 477
13. FX 71-L-150/30
14. Joukowsky 16.00% thick 1.00% camber
15. EPPLER 169
16. FX 71-L-150/20
17. Joukowsky 17.00% thick 1.00% camber
18. FX 71-L-150/25
19. NACA0015
20. GA 30-015
21. GA 35-016