Similarly shaped airfoils to TsAGI B 6.0% thick
New! Bulk download of polars in Excel format: TsAGI%20B%206.0%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. BOEING VERTOL V13006-.7
3. ONERA OA206
4. EH 1.0/7.0
5. GOE 598
6. TsAGI B 7.0% thick
7. RAF 25
8. NACA22007
9. D6213-S
10. BOEING-VERTOL VR-9
11. PW2019 tip airfoil 3m
12. SIKORSKY SSC-A07
13. NACA22107
14. salazV3root
15. HT23
16. MJP712
17. FAD17
18. TP100
19. MB7136
20. salazV3tip
21. NACA22005