Similarly shaped airfoils to NACA65A316
New! Bulk download of polars in Excel format: NACA65A316.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. NACA66-316 a=0.8
3. NACA66A316
4. NACA66-416
5. NACA65-316 a=0.8
6. NACA65A317
7. NACA65A315
8. NACA66-316 a=0.6
9. NACA65-416
10. GA 37A216
11. GA 40A216
12. NACA65-316 a=0.6
13. NACA64A317
14. NACA66-316
15. NACA65-317 a=0.8
16. NACA66A315
17. NACA66-315 a=0.8
18. NACA66-316 a=0.5
19. GA 40-216
20. NACA65-417
21. NACA63A316