Similarly shaped airfoils to NACA64-614
New! Bulk download of polars in Excel format: NACA64-614.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. NACA63-614
3. NACA63-514 a=0.8
4. NACA63A514
5. NACA65-614
6. HQ 3.0/14
7. NACA65-514 a=0.8
8. NACA64A514
9. NACA63A513
10. NACA64-615
11. NACA64-613
12. S4233-136-84
13. MH 201 13.08%
14. NACA64-513 a=0.8
15. NACA64-515 a=0.8
16. NACA63-613
17. NACA64-514 a=0.6
18. NACA63-615
19. NACA64A513
20. HQ 3.0/13
21. GA 37-414