Similarly shaped airfoils to NACA35016


New! Bulk download of polars in Excel format: NACA35016.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. NACA35016.5
2. NACA45016
3. NACA44016
4. NACA45016.5
5. NACA44016.5
6. NACA35017
7. NACA35015
8. NACA45017
9. NACA45015
10. NACA44015
11. TsAGI B 15.5% thick
12. Horten 16.00% thick 4.00% camber
13. TsAGI B 16.0% thick
14. NACA44017
15. TsAGI B 15.0% thick
16. DAVIS BASIC B-24 WING
17. NACA35014.5
18. S8037 (16%)
19. TsAGI B 16.5% thick
20. NACA34016
21. NACA35116