Similarly shaped airfoils to EM J18 3012 DrW r1,2
New! Bulk download of polars in Excel format: EM%20J18%203012%20DrW%20r1%2C2.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. HQ 3.0/12
3. SB 96 12.7/3.0
4. EM L3 3012
5. SB96 11.6/3.0
6. NACA63-612
7. NACA63-512 a=0.8
8. NACA64-612
9. SB96D TRAINER
10. EM J18 3013
11. NACA64-512 a=0.8
12. NACA63-613
13. NACA63A512
14. NACA63-712
15. CLARK X
16. CB3512
17. NACA63-513 a=0.8
18. HQ 3.0/13
19. CLARK K
20. EPPLER 854
21. HQ 3.5/12