Similarly shaped airfoils to Bambino 6
New! Bulk download of polars in Excel format: bambino6.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. BOEING-VERTOL VR-11X
3. GA 37A313
4. GA 30A313
5. GA 35A313
6. LOCKHEED L-188 TIP
7. GA 30A312
8. GA 37A413
9. NACA67-512 a=0.2
10. RAF 38
11. NACA66-512 a=0.2
12. FAD24
13. Jedeslsky EJ1
14. GA 30A413
15. Ritz 3-30-12
16. NACA66-513 a=0.2
17. GA 35A413
18. NACA66-512 a=0.0
19. BOEING 106
20. NACA66-412 a=0.5
21. NACA67-412 a=0.5