Similarly shaped airfoils to EM CY 1016 20145
New! Bulk download of polars in Excel format: EM%20CY%201016%2020145.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. NACA63-415
3. NACA64-415
4. CB2514
5. NACA63A415
6. LOCKHEED L-188 ROOT
7. AVISTAR
8. NACA63-515
9. NACA64-515
10. GA 30-314
11. MID 327 15%
12. NACA63-415 a=0.8
13. NACA64-415 a=0.8
14. EM J18 2515 DrW r0,8
15. GA 30-214
16. NACA63A315
17. NACA63-315 a=0.8
18. CB2515
19. GA 35A315
20. NACA64-315 a=0.8
21. NACA63A414