Similarly shaped airfoils to NACA23016
New! Bulk download of polars in Excel format: NACA23016.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (37) | 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. NACA23116
3. NACA23016.5
4. NACA24016
5. NACA22016
6. NACA23116.5
7. NACA24016.5
8. Horten 16.00% thick 1.00% camber
9. NACA24116
10. NACA25016
11. NACA23017
12. NACA23015
13. NACA24116.5
14. NACA25016.5
15. NACA23115
16. NACA42016
17. NACA23117
18. NACA24017
19. NACA22015
20. NACA22115
21. NACA32015