Similarly shaped airfoils to EM J8 3010 DrW


New! Bulk download of polars in Excel format: EM%20J8%203010%20DrW.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 J19 3010
2. SB96 10.5/3.0
3. HQ 3.0/10
4. NACA63-610
5. EM J18 3010 26 51
6. NACA63-510 a=0.8
7. NACA64-610
8. HS 602
9. NACA64-510 a=0.8
10. NACA63A510
11. S7075 (9%)
12. NACA63-611
13. NM Classic 12 saumon
14. EM J18 2610 27 48
15. EM J8 2510 DrW
16. NACA64A510
17. EM L3 2510
18. NACA63-511 a=0.8
19. SA7036
20. NACA64-611
21. HQ 3.0/9