Similarly shaped airfoils to LOCKHEED C-141 BL0


New! Bulk download of polars in Excel format: c141a.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
Dynamic plotter New!
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.

1. LOCKHEED C-141 BL113.6
2. NACA65A214
3. NACA65A213
4. NACA64A214
5. NACA66-213
6. NACA66A213
7. NACA66-213 a=0.8
8. RC12-64C
9. NACA67A213
10. NACA63A214
11. NACA66A214
12. NACA67-213
13. NACA67-213 a=0.8
14. NACA66-214
15. NACA66-214 a=0.8
16. NACA66-213 a=0.6
17. NACA64A213
18. NACA65A114
19. NACA67-213 a=0.6
20. NACA66-214 a=0.6
21. NACA66-213 a=0.5