Similarly shaped airfoils to TsAGI B 11.5% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2011.5%25%20thick.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. TsAGI B 12.0% thick
3. TsAGI B 11.0% thick
4. NACA 2R212
5. NACA M6
6. EPPLER 361
7. NACA25012
8. GOE 677 (= M 6)
9. EPPLER 360
10. RC-12(N)1
11. NACA24012
12. Europa Dykins 12%
13. NACA 2R112
14. RAF 34
15. TsAGI B 12.5% thick
16. TsAGI B 10.5% thick
17. EH 2.0/12
18. NACA2212
19. NACA25112
20. NACA65-312 a=0.0
21. GOE 676 (= M 12)