Similarly shaped airfoils to TsAGI B 10.5% thick
New! Bulk download of polars in Excel format: TsAGI%20B%2010.5%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 10.0% thick
3. ZAGI 10
4. AMES A-01
5. RC-10(B)3
6. NACA25010.5
7. NACA24010.5
8. Sipkill 1.7/10
9. LOCKHEED-GEORGIA SUPERCRITICAL
10. NACA65-311 a=0.0
11. TsAGI B 11.5% thick
12. TsAGI B 9.5% thick
13. BOEING 737 OUTBOARD
14. Horten 11.00% thick 2.00% camber
15. KC-135 BL200.76
16. NACA64-311 a=0.0
17. AMES A-03
18. FX 69-H-098
19. NACA23010.5
20. RC-10(N)1
21. NACA65-311 a=0.2