Similarly shaped airfoils to NACA64A410
New! Bulk download of polars in Excel format: NACA64A410.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA65-410 a=0.8
3. NACA65A410
4. NACA65-510
5. NACA64-410 a=0.8
6. NACA64-510
7. NACA63-410 a=0.8
8. NACA65-410 a=0.6
9. GA 37A310
10. NACA63-510
11. GA 35A310
12. HQ 2.5/10
13. NACA65-410
14. NACA64-410 a=0.6
15. GA 40A310
16. NACA64-411 a=0.8
17. GA 40-310
18. EPPLER 852
19. NACA65A409
20. HN-1023
21. NACA64A411