Similarly shaped airfoils to EM J18 3010 26 51
New! Bulk download of polars in Excel format: EM%20J18%203010%2026%2051.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
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. EM J8 3010 DrW
3. HS 602
4. SB96 10.5/3.0
5. FX 60-100 10.0% smoothed
6. HQ 3.0/10
7. EM J18 3510 26 51
8. S7075 (9%)
9. NACA63-610
10. EM J18 2610 27 48
11. Joukowsky 10.00% thick 3.00% camber
12. AH 79-100 A
13. SA7036
14. FX 60-100
15. NACA63-510 a=0.8
16. SA7038
17. NM Classic 12 saumon
18. EM L3 2510
19. EM J18 2510 26 51
20. OAF102
21. WASP (smoothed)