Similarly shaped airfoils to TsAGI B 9.5% thick
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. ONERA OA209
8. NACA24010
9. Horten 10.00% thick 2.00% camber
10. NACA23010
11. NACA65-210 a=0.2
12. NACA25010
13. FX 69-H-098
14. SIKORSKY SSC-A09
15. NACA64-210 a=0.2
16. TsAGI B 8.5% thick
17. TsAGI B 10.5% thick
18. EH 2.0/10
19. NACA65-210 a=0.0
20. LOCKHEED-GEORGIA SUPERCRITICAL
21. KC-135 BL200.76