Similarly shaped airfoils to S4061-096-84
New! Bulk download of polars in Excel format: s4061.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. S3025 9.38%
3. EPPLER 387
4. NACA63-510 a=0.6
5. NACA63-510 a=0.5
6. GOE 115 (MVA MK.2)
7. SA7038
8. MID 321b
9. EPPLER 174
10. EPPLER E193gU-K24
11. MH 38 9.68%
12. S3024 9.84%
13. EPPLER 193
14. NACA4409
15. GA 35-410
16. NACA63-509 a=0.6
17. NACA63-509 a=0.5
18. NACA64-510 a=0.6
19. MID 321c
20. MID 321a
21. NACA64-510 a=0.5