Similarly shaped airfoils to NACA66-312
New! Bulk download of polars in Excel format: NACA66-312.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. NACA66-212 a=0.8
3. NACA66A312
4. NACA66-212 a=0.6
5. NACA66A212
6. NACA66-312 a=0.8
7. NACA66-212 a=0.5
8. NACA66(1)-212
9. NACA65A312
10. NACA65A212
11. CAST 10-2/DOA 2
12. NACA66-312 a=0.6
13. NACA66-313
14. NACA66-311
15. NACA66-312 a=0.5
16. NACA66-312 a=0.0
17. NACA66-212
18. NACA65-312
19. NACA66-412
20. NACA66-312 a=0.2
21. NACA67A312