Similarly shaped airfoils to TsAGI B 18.0% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2018.0%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 18.5% thick
3. TsAGI B 17.0% thick
4. TsAGI B 19.0% thick
5. NACA45018
6. TsAGI B 16.5% thick
7. TsAGI B 19.5% thick
8. NACA45019
9. GOE 683
10. NACA65-519 a=0.2
11. NACA65-519 a=0.0
12. NACA44018
13. NACA65-619 a=0.0
14. GA 35A319
15. GA 37A319
16. NACA35017
17. NACA64-619 a=0.0
18. NACA64-519 a=0.2
19. GOE 703
20. NACA45017
21. NACA35018