Similarly shaped airfoils to CAL4014l
New! Bulk download of polars in Excel format: CAL4014l.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. MH 60 10.08%
3. S5010
4. MH 62 9.3%
5. HUGHES HELICOPTERS HH-02
6. EPPLER 221
7. MH 44 9.66%
8. MH 20 9.01%
9. MH 42 8.94%
10. MH 46 9.1%
11. EH 2.0/10
12. MH 61 10.26%
13. EH 2.5/10
14. NACA25009
15. NACA63-310 a=0.2
16. NACA63-310 a=0.0
17. B-29 TIP
18. NACA2209
19. NACA24009
20. NACA25010
21. NACA25109