Similarly shaped airfoils to NACA22019
New! Bulk download of polars in Excel format: NACA22019.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. NACA23119
3. NACA32019
4. NACA22018
5. NACA22118
6. NACA32119
7. NACA32018
8. NACA32118
9. Horten 19.00% thick 1.00% camber
10. NACA42119
11. NACA23019
12. NACA23018.87
13. NACA42019
14. GA 30A019
15. GA 30-019
16. NACA33019
17. Horten 20.00% thick 1.00% camber
18. Horten 19.00% thick 0.00% camber
19. GA 30A018
20. GA 30-018
21. Horten 19.00% thick 2.00% camber