Similarly shaped airfoils to NACA65-412
New! Bulk download of polars in Excel format: NACA65-412.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(1)-412
3. NACA65-312 a=0.6
4. NACA64-412
5. NACA64A312
6. NACA63A312
7. NACA64-312 a=0.8
8. NACA65A312
9. NACA65-312 a=0.5
10. NACA64A412
11. NACA65-413
12. NACA65-411
13. NACA65-412 a=0.8
14. NACA64-312 a=0.6
15. NACA63-412
16. GA 40-212
17. GA 40A212
18. NACA63A412
19. NACA64-413
20. NACA65-311 a=0.8
21. NACA65A311