Similarly shaped airfoils to TsAGI B 13.5% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2013.5%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 14.0% thick
3. GOE 704
4. TsAGI B 12.5% thick
5. TsAGI B 14.5% thick
6. GOE 617
7. NACA25113.5
8. NACA25014
9. NACA25013.5
10. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
11. NACA25014.5
12. NACA65-414 a=0.0
13. NACA25113
14. NACA 747A315
15. NACA25013
16. NACA65-314 a=0.2
17. EPPLER 327
18. GA 35A214
19. GA 37A214
20. NACA64-414 a=0.0
21. NACA34014