Similarly shaped airfoils to EPPLER 186
New! Bulk download of polars in Excel format: e186.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. HM391-2
3. NACA22110
4. Horten 10.00% thick 1.00% camber
5. NACA22010
6. MH 110 10.01%
7. NACA23110.5
8. Horten 10.00% thick 2.00% camber
9. NACA22110.5
10. NACA22010.5
11. NACA22109
12. Horten 9.00% thick 1.00% camber
13. EH 1.0/9.0
14. NACA23110
15. MH 61 10.26%
16. GIII BL86
17. NACA63-110 a=0.2
18. EH 1.5/9.0
19. GIII BL75
20. NACA63-210 a=0.0
21. NACA63-110 a=0.0