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
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. 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