Similarly shaped airfoils to NACA63-519


Direct link: NACA63-519
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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1. NACA63-419 a=0.8
2. NACA64-519
3. NACA64-419 a=0.8
4. NACA63-419 a=0.6
5. GA 35-319
6. NACA63-520
7. NACA63-518
8. NACA63-418 a=0.8
9. NACA64-419 a=0.6
10. NACA63-420 a=0.8
11. NACA63-419
12. NACA63-619
13. NACA63(3)-418
14. NACA64-619
15. NACA63-419 a=0.5
16. NACA64-518
17. GA 37-319
18. NACA64-520
19. NACA64-418 a=0.8
20. NACA64(3)-418
21. NACA64-420 a=0.8