Similarly shaped airfoils to NACA63A520
New! Bulk download of polars in Excel format: NACA63A520.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. NACA63A519
3. NACA65-520 a=0.8
4. NACA65-620
5. NACA64A519
6. NACA64-520 a=0.8
7. GA 35A420
8. GA 35A320
9. NACA64-620
10. NACA63A420
11. NACA63A620
12. NACA64A420
13. GA 37A420
14. GA 37A320
15. NACA65-520 a=0.6
16. NACA64A620
17. NACA64-720
18. NACA64-520 a=0.6
19. NACA65A520
20. NACA65-520
21. NACA63-520 a=0.8