Similarly shaped airfoils to EM J18 3013


New! Bulk download of polars in Excel format: EM%20J18%203013.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. SB96D TRAINER
2. SB 96 12.7/3.0
3. HQ 3.0/13
4. NACA63-613
5. EPPLER 854
6. NACA63-513 a=0.8
7. MS3,3-13GP
8. CB3013
9. NACA64-613
10. EM J18 3012 DrW r1,2
11. MS3/13GPV
12. HN-975TA
13. EPPLER 68
14. NACA63-614
15. NACA64-513 a=0.8
16. EM J18 3212
17. SB99A22C4
18. NACA63A513
19. NACA63-514 a=0.8
20. EM L3 3012
21. HQ 3.0/12