Similarly shaped airfoils to NACA63A519
New! Bulk download of polars in Excel format: NACA63A519.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. NACA63A520
3. NACA63A518
4. NACA65-519 a=0.8
5. NACA64A520
6. NACA65-619
7. NACA64-519 a=0.8
8. NACA64A518
9. NACA64-520 a=0.8
10. NACA64-619
11. NACA64-620
12. GA 35A419
13. NACA63A419
14. GA 35A319
15. GA 37A419
16. NACA63A619
17. NACA65-520 a=0.8
18. NACA64A419
19. NACA65-620
20. GA 37A319
21. NACA65-519 a=0.6