Similarly shaped airfoils to Borge-b3
New! Bulk download of polars in Excel format: Borge-b3.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. Horten 11.00% thick 2.00% camber
3. EH 2.0/12
4. JWL067 11.5/1.7
5. NACA24112
6. GOE 766
7. MJZ1211
8. NACA24012
9. HM391-1
10. NACA23112
11. MH 108 11.98%
12. EPPLER 361
13. NACA32012
14. NACA23012
15. NACA63-212 a=0.2
16. NACA63-212 a=0.0
17. Horten 11.00% thick 1.00% camber
18. NACA63-312 a=0.0
19. REPUBLIC S-3
20. NACA24110.5
21. NACA 2R212