Similarly shaped airfoils to NACA45016
New! Bulk download of polars in Excel format: NACA45016.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
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2. NACA35016
3. NACA35016.5
4. NACA44016
5. NACA45017
6. NACA45015
7. NACA44016.5
8. Horten 16.00% thick 4.00% camber
9. NACA35017
10. NACA35015
11. NACA44015
12. NACA35116
13. NACA44017
14. NACA35116.5
15. Horten 15.00% thick 4.00% camber
16. NACA35115
17. TsAGI B 16.0% thick
18. NACA35014.5
19. TsAGI B 15.5% thick
20. Horten 16.00% thick 5.00% camber
21. NACA44014.5