Similarly shaped airfoils to EM J18 1 3015


New! Bulk download of polars in Excel format: EM%20J18%201%203015.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
Dynamic plotter New!
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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. EM J18 3015 DrW r0,8
2. HQ 3.0/15
3. NACA63(2)-615
4. NACA63-715
5. NACA63-615
6. MS3,3-15GP
7. GOE 493
8. NACA63-515 a=0.8
9. USA 48
10. NACA64-715
11. NACA63-716
12. HQ 3.0/14
13. NACA64-615
14. MS3/15GPV
15. NACA63-616
16. NACA64-515 a=0.8
17. FX 60-160
18. NACA64-716
19. NACA63-516 a=0.8
20. EPPLER 556
21. NACA63A515