Similarly shaped airfoils to NACA23019
New! Bulk download of polars in Excel format: NACA23019.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (5) | 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. NACA24019
3. Horten 19.00% thick 2.00% camber
4. Horten 19.00% thick 1.00% camber
5. NACA24119
6. NACA25019
7. NACA23018
8. NACA23118
9. NACA33019
10. NACA2219
11. NACA42019
12. NACA24018
13. Horten 20.00% thick 2.00% camber
14. Horten 20.00% thick 1.00% camber
15. Horten 18.00% thick 1.00% camber
16. NACA23119
17. NACA24118
18. NACA25018
19. NACA42018
20. NACA32019
21. NACA25119