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
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
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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