Similarly shaped airfoils to NACA64-514
New! Bulk download of polars in Excel format: NACA64-514.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (9) | 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. NACA63-514
3. NACA63-414 a=0.8
4. NACA64-414 a=0.6
5. NACA63A414
6. NACA65-514
7. EPPLER 203
8. NACA65-414 a=0.8
9. GA 37-314
10. NACA63-414 a=0.6
11. NACA64A414
12. NACA63A413
13. NACA64-515
14. NACA64-513
15. GA 35-314
16. NACA64-413 a=0.8
17. NACA64-415 a=0.8
18. NACA63-513
19. NACA63-515
20. NACA64-414
21. NACA64A413