Similarly shaped airfoils to NACA65A314
New! Bulk download of polars in Excel format: NACA65A314.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. NACA66A314
3. NACA66-314 a=0.8
4. NACA65-314 a=0.8
5. NACA66-414
6. NACA66-314 a=0.6
7. NACA65-414
8. LOCKHEED L-188 ROOT
9. NACA65-314 a=0.6
10. NACA65A315
11. NACA65A313
12. NACA66-314
13. NACA63A314
14. GA 37A214
15. GA 40A214
16. NACA65-315 a=0.8
17. NACA66-314 a=0.5
18. NACA64A315
19. NACA65-314
20. NACA66A313
21. NACA66-313 a=0.8