Similarly shaped airfoils to EM J18 2515 DrW r0,8
New! Bulk download of polars in Excel format: EM%20J18%202515%20DrW%20r0%2C8.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. NACA64-515
3. MS2.5/15GPV
4. CB2515
5. NACA63-415 a=0.8
6. NACA63-516
7. MID 327 15%
8. CB2514
9. NACA64(2)-415
10. NACA63-615
11. USA 48
12. NACA64-415 a=0.8
13. NACA63A415
14. EM J18 3015 DrW r0,8
15. NACA64-615
16. NACA64-516
17. NACA63-616
18. EM CY 1016 20145
19. NACA63-416 a=0.8
20. MID 393 UL
21. NACA63-515 a=0.8