Similarly shaped airfoils to TsAGI B 18.5% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2018.5%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 18.0% thick
3. TsAGI B 17.5% thick
4. TsAGI B 19.5% thick
5. GOE 683
6. NACA45019
7. TsAGI B 17.0% thick
8. TsAGI B 20.0% thick
9. NACA45018
10. GOE 703
11. NACA65-520 a=0.2
12. NACA65-620 a=0.0
13. NACA65-519 a=0.2
14. NACA65-619 a=0.0
15. NACA65-519 a=0.0
16. NACA65-520 a=0.0
17. NACA64-620 a=0.0
18. GA 35A319
19. GA 37A319
20. GA 30A319
21. NACA64-520 a=0.2