Similarly shaped airfoils to NACA64A219
New! Bulk download of polars in Excel format: NACA64A219.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. NACA65-219 a=0.8
3. NACA65-219 a=0.6
4. NACA65-219
5. NACA65-219 a=0.5
6. NACA65-319
7. NACA64A220
8. NACA64A218
9. NACA65A219
10. NACA63A218
11. AS5048 (18%)
12. NACA65-220 a=0.8
13. NACA63A220
14. NACA65-219 a=0.2
15. NACA65-220 a=0.6
16. NACA65A218
17. NACA65-220
18. NACA64A119
19. NACA64A319
20. NACA65-220 a=0.5
21. NACA65-320