Similarly shaped airfoils to NACA64-519
New! Bulk download of polars in Excel format: NACA64-519.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. NACA63-519
3. NACA63-419 a=0.8
4. NACA64-419 a=0.6
5. GA 37-319
6. NACA64-520
7. NACA64-518
8. NACA63-419 a=0.6
9. NACA64-418 a=0.8
10. GA 35-319
11. NACA64-420 a=0.8
12. NACA64-419
13. NACA64-619
14. NACA64(3)-418
15. NACA63A418
16. NACA63-419
17. NACA64-419 a=0.5
18. NACA63-518
19. NACA63-520
20. NACA63-418 a=0.8
21. NACA63A419