Similarly shaped airfoils to NACA65-410
New! Bulk download of polars in Excel format: NACA65-410.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA64-410
3. NACA64A310
4. NACA65-310 a=0.6
5. NACA64-310 a=0.8
6. SB98 VS5 tip
7. NACA65A310
8. NACA63A310
9. NACA63-410
10. NACA65-310 a=0.5
11. NACA64-310 a=0.6
12. NACA66-410
13. NACA64A410
14. EM CY 1025 20098
15. HQ 2.0/10
16. NACA63-310 a=0.8
17. NACA65-411
18. NACA63A410
19. NACA65-409
20. NACA65-410 a=0.8
21. NACA64-411