Similarly shaped airfoils to NACA64-412
New! Bulk download of polars in Excel format: NACA64-412.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (33) | 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. NACA64-312 a=0.8
3. NACA63-312 a=0.8
4. NACA64-312 a=0.6
5. HQ 2.0/12
6. NACA65-412
7. NACA63-312 a=0.6
8. NACA65-312 a=0.8
9. NACA63A312
10. EM CY 1016 2012
11. NACA64A312
12. NACA64-312 a=0.5
13. NACA65(1)-412
14. NACA65-312 a=0.6
15. NACA63-312 a=0.5
16. NACA64-413
17. NACA64-411
18. SB95 11.5/2
19. GA 37-212
20. EM S5 1811 121
21. NACA64-412 a=0.8