Similarly shaped airfoils to BOEING BACXXX
New! Bulk download of polars in Excel format: bacxxx.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-141 BL426.57
3. LOCKHEED C-141 BL610.61
4. LOCKHEED C-5A BL758.6
5. NACA64A212
6. NACA63A212
7. ONERA NACA CAMBRE
8. NACA65A211
9. GA 37A212
10. NACA65A212
11. NACA65(1)-212 a=0.6
12. LOCKHEED C-5A BL576
13. BOEING 737 OUTBOARD
14. NACA65-312
15. NACA64A211
16. GA 35A212
17. LOCKHEED C-5A BL1256
18. NACA63A211
19. NACA65(1)-212
20. NACA65-212 a=0.8
21. HQ 1.5/12