Similarly shaped airfoils to EM J18 3015 DrW r0,8
New! Bulk download of polars in Excel format: EM%20J18%203015%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. HQ 3.0/15
3. NACA63-615
4. USA 48
5. NACA63(2)-615
6. NACA63-515 a=0.8
7. GOE 493
8. NACA64-615
9. NACA63-715
10. MS3,3-15GP
11. NACA63-616
12. NACA64-515 a=0.8
13. NACA63A515
14. HQ 3.0/14
15. MS3/15GPV
16. NACA64-715
17. NACA63-716
18. EM J18 2515 DrW r0,8
19. NACA63-516 a=0.8
20. FX 60-160
21. NACA64-616