Similarly shaped airfoils to NACA64-310 a=0.6
New! Bulk download of polars in Excel format: NACA64-310%20a%3D0.6.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. NACA63-310 a=0.6
3. NACA63-310 a=0.5
4. NACA64-310 a=0.8
5. NACA65-310 a=0.6
6. NACA63-310 a=0.8
7. NACA65-310 a=0.5
8. GA 37-210
9. NACA64-410
10. NACA63-410
11. NACA63A310
12. SB98 VS5 tip
13. GA 35-210
14. SB95 9.5/2
15. NACA65-310 a=0.8
16. GA 35A210
17. GA 40-210
18. HQ 2.0/10
19. NACA64A310
20. GA 40A210
21. RAF 28