Similarly shaped airfoils to LOCKHEED C-141 BL113.6
New! Bulk download of polars in Excel format: c141b.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. NACA65A213
3. RC12-64C
4. NACA65A214
5. NACA66A213
6. NACA66-213 a=0.8
7. NACA66-213
8. NACA64A213
9. NACA64A214
10. LOCKHEED C-5A BL488.2
11. NACA66-213 a=0.6
12. HAWKER TEMPEST 61% SEMISPAN
13. NACA63A213
14. NACA67A213
15. NACA67-213 a=0.8
16. NACA66-213 a=0.5
17. NACA63A214
18. NACA67-213
19. NACA66-313
20. CAST 10-2/DOA 2
21. NACA67A212