Similarly shaped airfoils to RC-10(B)3
New! Bulk download of polars in Excel format: rc10b3.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 10.5% thick
3. TsAGI B 10.0% thick
4. ZAGI 10
5. NACA67-310 a=0.0
6. NACA66-310 a=0.0
7. BOEING 737 OUTBOARD
8. AMES A-01
9. NACA67-310 a=0.2
10. TsAGI B 11.0% thick
11. FX 69-H-098
12. NACA66-310 a=0.2
13. NACA66-311 a=0.0
14. NACA65-311 a=0.0
15. NACA66-311 a=0.2
16. LOCKHEED-GEORGIA SUPERCRITICAL
17. TsAGI B 9.5% thick
18. Sipkill 1.7/10
19. KC-135 BL200.76
20. NACA65-311 a=0.2
21. GA 37A211