Similarly shaped airfoils to RC(5)-10
New! Bulk download of polars in Excel format: rc510.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. BOEING-VERTOL VR-13
3. NACA25010
4. NACA64-410 a=0.0
5. NACA25110
6. NACA63-410 a=0.0
7. RC_Milan
8. EH 2.5/10
9. NACA64-411 a=0.0
10. NACA2210
11. NACA63-411 a=0.0
12. SIKORSKY SC2110
13. JWL077 10/2
14. NACA65-410 a=0.0
15. NACA25010.5
16. ZAGI 10
17. NACA33010
18. NACA25110.5
19. SIKORSKY SC1094 R8
20. SD6060-104-88
21. NACA 5-H-10