Similarly shaped airfoils to FX 082-512


New! Bulk download of polars in Excel format: fx082512.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. AF5600k
2. OAF102
3. NACA2012 AF512-OP
4. MID 107
5. EPPLER 212
6. FX 60-100 (126)
7. MH 122 9.32%
8. AH 79-100 A
9. EPPLER 853
10. FX 83-W-108
11. FX 60-126
12. FX 60-100 10.0% smoothed
13. FX 60-100
14. HS 602
15. Joukowsky 11.00% thick 4.00% camber
16. OAF095
17. Joukowsky 12.00% thick 4.00% camber
18. EM J19 3010
19. SB96 10.5/3.0
20. EPPLER 818 HYDROFOIL
21. Joukowsky 11.00% thick 3.00% camber