Similarly shaped airfoils to EPPLER 854


New! Bulk download of polars in Excel format: e854.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 3013
2. SB96D TRAINER
3. NACA63-613
4. NACA63-713
5. EPPLER 68
6. SB 96 12.7/3.0
7. NACA64-613
8. HQ 3.0/13
9. NACA63-513 a=0.8
10. NACA64-713
11. NACA64-513 a=0.8
12. NACA63-714
13. NACA63A513
14. NACA63-614
15. EM J18 3012 DrW r1,2
16. NACA64-714
17. NACA64-614
18. NACA63-514 a=0.8
19. EM J18 3212
20. NACA63-613 a=0.8
21. NACA63A613