Similarly shaped airfoils to NACA65-310
New! Bulk download of polars in Excel format: NACA65-310.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. NACA65-210 a=0.8
3. NACA65-210 a=0.6
4. GA 40-210
5. GA 40A210
6. NACA64A310
7. NACA65-310 a=0.8
8. SB96VS 9.75/1.25
9. GA 37A210
10. NACA63A310
11. NACA65-210 a=0.5
12. NACA64A210
13. NACA63-310
14. NACA65A310
15. NACA64-210 a=0.8
16. GA 35A210
17. NACA63A210
18. NACA65A210
19. NACA66-310
20. EM CY 1016 1510
21. NACA64-210 a=0.6