Similarly shaped airfoils to NACA64A211
New! Bulk download of polars in Excel format: NACA64A211.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. NACA65-211 a=0.8
3. NACA65-211 a=0.6
4. NACA65A211
5. NACA65-211
6. NACA65-211 a=0.5
7. NACA64-211 a=0.8
8. NACA64-211 a=0.6
9. NACA64-211
10. NACA64-211 a=0.5
11. LOCKHEED C-5A BL1256
12. NACA65-311
13. NACA65-211 a=0.2
14. NACA63-211 a=0.8
15. BOEING-VERTOL VR-1
16. NACA64-311
17. NACA63-211 a=0.6
18. NACA65-211 a=0.0
19. NACA64-212 a=0.8
20. NACA65A210
21. NACA64A212