Similarly shaped airfoils to TsAGI B 12.0% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2012.0%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
Dynamic plotter New!
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. NACA M6
3. NACA M6 (NACA-TR-221)
4. TsAGI B 11.5% thick
5. TsAGI B 12.5% thick
6. GOE 677 (= M 6)
7. NACA 2R212
8. RAF 34
9. NACA M12 (NACA-TR-221)
10. EPPLER 361
11. NACA25012
12. EPPLER 360
13. NACA 2R112
14. GOE 676 (= M 12)
15. Europa Dykins 12%
16. ONERA OA212
17. TsAGI B 13.0% thick
18. TsAGI B 11.0% thick
19. NACA M12
20. NACA25112
21. NACA25013