Similarly shaped airfoils to EM J19 3010
New! Bulk download of polars in Excel format: EM%20J19%203010.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.
2. SB96 10.5/3.0
3. EM J18 3010 26 51
4. NACA63-610
5. HQ 3.0/10
6. HS 602
7. NACA63-510 a=0.8
8. NACA64-610
9. S7075 (9%)
10. NACA64-510 a=0.8
11. NACA63A510
12. EM J18 2610 27 48
13. NACA63-611
14. EM L3 2510
15. EM J8 2510 DrW
16. NM Classic 12 saumon
17. FX 60-100 10.0% smoothed
18. HQ 3.0/9
19. SA7036
20. NACA63-511 a=0.8
21. EPPLER 212