Similarly shaped airfoils to RC-SC2


New! Bulk download of polars in Excel format: rcsc2.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
Dynamic plotter New!
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.

1. RC10-64C
2. NACA65A111
3. NACA64A111
4. HAWKER TEMPEST 96.77% SEMISPAN
5. NACA63A111
6. NACA65A110
7. GIII BL45
8. NACA67A110
9. NACA67-110 a=0.8
10. NACA67-110
11. NACA0010-64
12. NACA67-110 a=0.6
13. NACA66A110
14. NACA66-110 a=0.8
15. NACA66A111
16. NACA66-111 a=0.8
17. NACA65-111 a=0.8
18. NACA67-110 a=0.5
19. NACA66-110
20. NACA64A110
21. NACA66-111