Similarly shaped airfoils to NACA25019
New! Bulk download of polars in Excel format: NACA25019.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | 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. NACA2219
3. NACA25119
4. NACA24119
5. NACA23018.87
6. Horten 19.00% thick 2.00% camber
7. NACA23019
8. NACA25018
9. NACA24018
10. NACA2218
11. NACA24118
12. Horten 18.00% thick 2.00% camber
13. NACA25118
14. NACA23018
15. NACA34019
16. Horten 19.00% thick 1.00% camber
17. Horten 20.00% thick 2.00% camber
18. NACA33018
19. Horten 19.00% thick 3.00% camber
20. NACA23118
21. NACA33019