Similarly shaped airfoils to NACA23018
New! Bulk download of polars in Excel format: NACA23018.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (155) | 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. NACA24018
3. NACA23017.424
4. Horten 18.00% thick 1.00% camber
5. NACA23018.87
6. NACA24118
7. NACA25018
8. NACA23019
9. NACA23017
10. NACA23117
11. NACA24019
12. NACA42018
13. NACA2218
14. NACA24017
15. Horten 19.00% thick 2.00% camber
16. Horten 19.00% thick 1.00% camber
17. NACA33018
18. Horten 18.00% thick 2.00% camber
19. NACA25019
20. NACA24119
21. Horten 17.00% thick 1.00% camber