Similarly shaped airfoils to TsAGI B 19.5% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2019.5%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 20.0% thick
3. TsAGI B 20.5% thick
4. TsAGI B 18.5% thick
5. GOE 683
6. TsAGI B 21.0% thick
7. TsAGI B 18.0% thick
8. GOE 703
9. NACA45019
10. NACA65-620 a=0.0
11. NACA45021
12. NACA65-520 a=0.2
13. TsAGI B 17.5% thick
14. TsAGI B 21.5% thick
15. GA 35A320
16. GA 37A320
17. NACA65-620 a=0.2
18. GA 30A320
19. NACA65-520 a=0.0
20. GA 30-320
21. NACA64-620 a=0.0