Similarly shaped airfoils to NACA64A514
New! Bulk download of polars in Excel format: NACA64A514.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. NACA65-514 a=0.8
3. NACA65-614
4. NACA65A514
5. NACA64-514 a=0.8
6. NACA64-614
7. NACA64A515
8. NACA64A513
9. NACA63A513
10. GA 37A414
11. NACA65-515 a=0.8
12. NACA65A513
13. NACA65-514 a=0.6
14. NACA64-515 a=0.8
15. NACA63A515
16. NACA65-615
17. GA 35A414
18. NACA64-615
19. GA 40A414
20. NACA65-514
21. NACA63-514 a=0.8