Similarly shaped airfoils to LOCKHEED C-5A BL576
New! Bulk download of polars in Excel format: c5c.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. LOCKHEED C-141 BL426.57
3. LOCKHEED C-5A BL488.2
4. LOCKHEED C-141 BL610.61
5. NACA65A212
6. NACA65A211
7. NACA64A212
8. MH 26 10.99%
9. NACA67-211 a=0.8
10. NACA67A211
11. NACA66-211 a=0.8
12. CAST 10-2/DOA 2
13. NACA66-312
14. NACA66A211
15. NACA66-311
16. NACA66-212 a=0.8
17. NACA66A212
18. BOEING BACXXX
19. NACA66(1)-212
20. NACA63A212
21. BOEING-VERTOL VR-1