Similarly shaped airfoils to TsAGI B 15.0% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2015.0%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 15.5% thick
3. TsAGI B 14.0% thick
4. TsAGI B 16.0% thick
5. NACA 747A315
6. S8037 (16%)
7. NACA 5-H-15
8. NACA35015
9. NACA35016
10. GEMINI (smoothed)
11. NACA65-416 a=0.2
12. NACA65-416 a=0.0
13. S8036 (16%)
14. TsAGI B 13.5% thick
15. TsAGI B 16.5% thick
16. NACA25015
17. NACA64-416 a=0.2
18. NACA34015
19. NACA35014.5
20. DAVIS BASIC B-24 WING
21. NACA65-516 a=0.0