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.
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