Similarly shaped airfoils to NACA63A218
New! Bulk download of polars in Excel format: NACA63A218.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (8) | 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. AS5048 (18%)
3. NACA65-218 a=0.8
4. NACA63A219
5. NACA63A217
6. NACA65(3)-218
7. NACA65-218 a=0.6
8. NACA64A219
9. NACA65-218
10. NACA64-218 a=0.8
11. NACA64-219 a=0.8
12. NACA65-218 a=0.5
13. NACA64(3)-218
14. NACA64-218 a=0.6
15. NACA64A217
16. NACA64-219 a=0.6
17. NACA64-218
18. NACA64-218 a=0.5
19. NACA64-319
20. NACA65-318
21. NACA64-318