Similarly shaped airfoils to NACA23016.5
New! Bulk download of polars in Excel format: NACA23016.5.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (30) | 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. NACA23017
3. NACA23016
4. NACA24016.5
5. NACA23015.9
6. NACA23116
7. NACA23117
8. NACA24017
9. NACA22016
10. NACA24016
11. NACA23017.424
12. NACA24116.5
13. Horten 17.00% thick 1.00% camber
14. NACA25016.5
15. Horten 16.00% thick 1.00% camber
16. NACA24117
17. NACA25017
18. NACA24116
19. NACA42016.5
20. NACA25016
21. NACA42016