Similarly shaped airfoils to TsAGI B 9.5% thick
New! Bulk download of polars in Excel format: TsAGI%20B%209.5%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 9.0% thick
3. RC-10(N)1
4. Sipkill 1.7/10
5. ZAGI 10
6. BOEING 737 MIDSPAN
7. BW 05 02 09
8. ONERA OA209
9. NACA24010
10. Horten 10.00% thick 2.00% camber
11. NACA23010
12. NACA65-210 a=0.2
13. NACA25010
14. FX 69-H-098
15. SIKORSKY SSC-A09
16. NACA64-210 a=0.2
17. TsAGI B 8.5% thick
18. TsAGI B 10.5% thick
19. EH 2.0/10
20. NACA65-210 a=0.0
21. LOCKHEED-GEORGIA SUPERCRITICAL