Similarly shaped airfoils to NACA45016.5
New! Bulk download of polars in Excel format: NACA45016.5.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
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. NACA45016
3. NACA35016.5
4. NACA35017
5. NACA35016
6. NACA44016.5
7. NACA44016
8. NACA44017
9. Horten 16.00% thick 4.00% camber
10. NACA35116.5
11. NACA35116
12. NACA35117
13. NACA45018
14. NACA45015
15. TsAGI B 16.0% thick
16. TsAGI B 16.5% thick
17. NACA35015
18. NACA44015
19. Horten 16.00% thick 5.00% camber
20. NACA45116.5
21. Horten 17.00% thick 5.00% camber