Similarly shaped airfoils to LOCKHEED C-5A BL0
New! Bulk download of polars in Excel format: c5a.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. NACA65A114
3. GOE 411
4. NACA66-113
5. NACA0012-64
6. NACA66A113
7. NACA64A114
8. NACA66-113 a=0.8
9. GA 37A014
10. GOE 409
11. NACA66-114
12. NACA65-114
13. LS(1)-0013
14. EPPLER 836 HYDROFOIL
15. GA 40A014
16. NACA64A113
17. NACA66-113 a=0.6
18. NACA66-113 a=0.0
19. NACA67-113
20. GA 37A013
21. NACA66A114