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
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. 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