Similarly shaped airfoils to NACA23018.87


New! Bulk download of polars in Excel format: NACA23018.87.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA23019
2. NACA24019
3. Horten 19.00% thick 2.00% camber
4. Horten 19.00% thick 1.00% camber
5. NACA23018
6. NACA24119
7. NACA23118
8. NACA25019
9. NACA24018
10. NACA33019
11. NACA2219
12. NACA42019
13. Horten 18.00% thick 1.00% camber
14. Horten 20.00% thick 2.00% camber
15. Horten 20.00% thick 1.00% camber
16. NACA24118
17. NACA25018
18. NACA23119
19. NACA42018
20. NACA23017.424
21. NACA25119