Similarly shaped airfoils to NACA65-514
New! Bulk download of polars in Excel format: NACA65-514.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. NACA64A414
3. NACA65-414 a=0.6
4. NACA64-514
5. NACA63A414
6. NACA65A414
7. NACA64-414 a=0.8
8. GA 40-314
9. GA 40A314
10. NACA65-515
11. NACA65-513
12. NACA65-413 a=0.8
13. MH 200 12.97%
14. NACA65-415 a=0.8
15. NACA65A413
16. GA 37A314
17. NACA65-414
18. NACA65-414 a=0.5
19. NACA64A413
20. NACA65-614
21. NACA65(2)-415