Similarly shaped airfoils to NACA64A316
New! Bulk download of polars in Excel format: NACA64A316.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. NACA65-316 a=0.8
3. GA 37A216
4. GA 35A216
5. NACA65-416
6. NACA65-316 a=0.6
7. GA 40A216
8. NACA65A316
9. NACA65-316
10. GA 40-216
11. NACA65-316 a=0.5
12. NACA64A317
13. NACA64A315
14. NACA63A315
15. NACA64-316 a=0.8
16. NACA65-317 a=0.8
17. NACA65A315
18. S8036 (16%)
19. NACA63A317
20. NACA64-416
21. NACA65-417