Similarly shaped airfoils to S8035 (14%)
New! Bulk download of polars in Excel format: s8035.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. GA 30-014
3. GA 30A014
4. St. CYR 172 (Royer)
5. GA 30-013
6. GA 30A013
7. Horten 13.00% thick 0.00% camber
8. NACA0013
9. GA 35A014
10. NACA63A014
11. FX LIII-142 K 25
12. GA 35-014
13. Horten 15.00% thick 0.00% camber
14. EPPLER 474
15. Horten 14.00% thick 1.00% camber
16. GOE 459
17. GA 35-015
18. NACA63-015
19. FX 71-L-150/30
20. FX 71-L-150/25
21. NACA0015