Similarly shaped airfoils to TsAGI B 14.0% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2014.0%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
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 14.5% thick
3. TsAGI B 15.0% thick
4. TsAGI B 13.0% thick
5. GOE 617
6. NACA 747A315
7. GOE 704
8. NACA25014.5
9. NACA25014
10. NACA65-415 a=0.0
11. NACA25113.5
12. NACA25015
13. NACA34014
14. NACA64-415 a=0.0
15. NACA65-415 a=0.2
16. NACA34014.5
17. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
18. NACA35014.5
19. NACA65-414 a=0.0
20. NACA64-415 a=0.2
21. NACA25013.5