Similarly shaped airfoils to NACA35116.5


New! Bulk download of polars in Excel format: NACA35116.5.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

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1. NACA35117
2. NACA35116
3. Horten 16.00% thick 4.00% camber
4. Horten 17.00% thick 4.00% camber
5. Horten 17.00% thick 5.00% camber
6. NACA44116
7. NACA44016.5
8. NACA44116.5
9. Horten 16.00% thick 5.00% camber
10. NACA34116.5
11. NACA44017
12. NACA34116
13. NACA44016
14. NACA34117
15. NACA44117
16. NACA45016.5
17. NACA45017
18. NACA45016
19. NACA35118
20. NACA35115
21. NACA45116.5