Similarly shaped airfoils to NACA2219
New! Bulk download of polars in Excel format: NACA2219.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (3) | 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. NACA2218
4. NACA25018
5. NACA23018.87
6. NACA23019
7. NACA24018
8. NACA25119
9. NACA24119
10. Horten 19.00% thick 2.00% camber
11. Horten 18.00% thick 2.00% camber
12. Horten 19.00% thick 1.00% camber
13. NACA23018
14. NACA1420
15. NACA1418
16. NACA24118
17. NACA34019
18. NACA25118
19. NACA2318
20. NACA33018
21. Horten 20.00% thick 2.00% camber