Similarly shaped airfoils to SG6041_CMPLXFOIL


New! Bulk download of polars in Excel format: SG6041_CMPLXFOIL.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. NACA6711
2. NACA6710
3. SG6043
4. NACA6712
5. GOE 500
6. AH 79-100 C
7. Joukowsky 11.00% thick 6.00% camber
8. Joukowsky 12.00% thick 6.00% camber
9. MH 115 11.06%
10. EPPLER 216
11. Joukowsky 10.00% thick 6.00% camber
12. NACA6410
13. GOE 239 (MVA H.31)
14. EPPLER 395
15. GOE 501
16. AH 79-100 B
17. Joukowsky 11.00% thick 7.00% camber
18. Joukowsky 12.00% thick 7.00% camber
19. GOE 190 (MVA MK.18)
20. Joukowsky 13.00% thick 6.00% camber
21. AF104k