Similarly shaped airfoils to NACA23017.424


New! Bulk download of polars in Excel format: NACA23017.424.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA23017
2. NACA23117
3. NACA23018
4. NACA24017
5. NACA23118
6. NACA24018
7. NACA23016.5
8. Horten 17.00% thick 1.00% camber
9. NACA23116.5
10. Horten 18.00% thick 1.00% camber
11. NACA24117
12. NACA25017
13. NACA24118
14. NACA25018
15. NACA24016.5
16. NACA42017
17. NACA2218
18. NACA24116.5
19. NACA42018
20. NACA32017
21. Horten 18.00% thick 2.00% camber