Similarly shaped airfoils to TsAGI B 17.0% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2017.0%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 17.5% thick
3. TsAGI B 16.0% thick
4. TsAGI B 18.0% thick
5. NACA35017
6. NACA45017
7. NACA45018
8. NACA35016.5
9. TsAGI B 15.5% thick
10. TsAGI B 18.5% thick
11. NACA65-518 a=0.0
12. NACA44017
13. NACA45016.5
14. NACA65-518 a=0.2
15. NACA44018
16. NACA65-418 a=0.2
17. NACA64-518 a=0.0
18. NACA35018
19. NACA44016.5
20. GA 35A318
21. NACA65-517 a=0.0