Similarly shaped airfoils to NACA63A620
New! Bulk download of polars in Excel format: NACA63A620.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. NACA63A619
3. NACA65-620 a=0.8
4. NACA64A619
5. NACA65-720
6. NACA64-620 a=0.8
7. NACA63A520
8. GA 35A420
9. NACA63A720
10. NACA64A520
11. NACA64-720
12. GA 37A420
13. NACA64A720
14. NACA65A620
15. NACA65-620 a=0.6
16. NACA63-620 a=0.8
17. NACA65-520 a=0.8
18. NACA63A519
19. NACA64-620 a=0.6
20. GA 35A419
21. NACA63-720