Similarly shaped airfoils to LOCKHEED C-141 BL426.57
New! Bulk download of polars in Excel format: c141c.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. LOCKHEED C-5A BL576
3. LOCKHEED C-141 BL610.61
4. LOCKHEED C-5A BL488.2
5. NACA65A212
6. NACA65A211
7. MH 26 10.99%
8. BOEING-VERTOL VR-1
9. BOEING BACXXX
10. NACA64A212
11. NACA66-211 a=0.8
12. NACA66A211
13. NACA66-211 a=0.6
14. NACA67-211 a=0.8
15. NACA66-311
16. NACA67A211
17. NACA63A212
18. NACA66-211 a=0.5
19. NACA67-211 a=0.6
20. NACA64A211
21. MH 25 9.98%