Similarly shaped airfoils to NACA63-711
New! Bulk download of polars in Excel format: NACA63-711.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. NACA63-611 a=0.8
3. NACA64-611 a=0.8
4. NACA63A611
5. NACA65-711
6. SG6042
7. GOE 546
8. NACA63-712
9. NACA63-710
10. NACA64A611
11. EPPLER 393
12. RAF 32 MOD
13. NACA64-710
14. NACA64-712
15. HQ 3.5/10
16. NACA63A610
17. NACA65-611 a=0.8
18. NACA63-511 a=0.8
19. NACA63-612 a=0.8
20. NACA63-611
21. NACA64-511 a=0.8