Similarly shaped airfoils to LOCKHEED C-141 BL761.11
New! Bulk download of polars in Excel format: c141e.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. NACA65A311
3. NACA64A311
4. BOEING-VERTOL VR-1
5. NACA63A311
6. NACA66A311
7. NACA66-311 a=0.8
8. LOCKHEED C-141 BL426.57
9. SG6041
10. AMSOIL1 RUTAN CANARD
11. LOCKHEED C-5A BL758.6
12. NACA66-411
13. LOCKHEED C-141 BL958.89
14. NACA64A312
15. GA 30A211
16. NACA65A312
17. MH 25 9.98%
18. GA 37A211
19. NACA66-311 a=0.6
20. MH 26 10.99%
21. NACA66-311