Similarly shaped airfoils to LOCKHEED C-141 BL610.61
New! Bulk download of polars in Excel format: c141d.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 BL761.11
3. LOCKHEED C-5A BL758.6
4. LOCKHEED C-5A BL576
5. BOEING-VERTOL VR-1
6. MH 26 10.99%
7. NACA65A311
8. BOEING BACXXX
9. NACA66-311
10. MH 25 9.98%
11. NACA65A211
12. NACA65A312
13. NACA64A312
14. NACA64A311
15. NACA66A311
16. LOCKHEED C-5A BL1256
17. NACA66-311 a=0.8
18. NACA66-211 a=0.8
19. GA 37A212
20. NACA66-211 a=0.6
21. NACA63A311