Similarly shaped airfoils to NACA23119
New! Bulk download of polars in Excel format: NACA23119.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. NACA22119
3. NACA32119
4. NACA22019
5. NACA32018
6. NACA33019
7. NACA22118
8. NACA42019
9. NACA32118
10. NACA22018
11. NACA42119
12. NACA23019
13. NACA23018.87
14. NACA33119
15. Horten 19.00% thick 2.00% camber
16. Horten 19.00% thick 1.00% camber
17. NACA42018
18. NACA23118
19. Horten 20.00% thick 2.00% camber
20. NACA42118
21. Horten 20.00% thick 1.00% camber