Similarly shaped airfoils to LOCKHEED C-5A BL488.2
New! Bulk download of polars in Excel format: c5b.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 BL758.6
3. LOCKHEED C-141 BL426.57
4. NACA65A212
5. AMSOIL2 RUTAN WING
6. NACA66(1)-212
7. HAWKER TEMPEST 61% SEMISPAN
8. NACA66-212
9. NACA66A212
10. NACA66-212 a=0.8
11. NACA64A212
12. CAST 10-2/DOA 2
13. LOCKHEED C-141 BL113.6
14. RC12-64C
15. NACA63A212
16. NACA65A213
17. NACA 66,2-(1.8)12 A=.6 P-51 TIP
18. LOCKHEED C-141 BL610.61
19. NACA67-211
20. NACA64A213
21. NACA65(1)-212