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
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. MID 107
3. EPPLER 212
4. FX 60-100 (126)
5. MH 122 9.32%
6. AH 79-100 A
7. EPPLER 853
8. FX 83-W-108
9. FX 60-126
10. FX 60-100 10.0% smoothed
11. FX 60-100
12. HS 602
13. Joukowsky 11.00% thick 4.00% camber
14. OAF095
15. Joukowsky 12.00% thick 4.00% camber
16. EM J19 3010
17. SB96 10.5/3.0
18. EPPLER 818 HYDROFOIL
19. Joukowsky 11.00% thick 3.00% camber
20. EM J18 3510 26 51
21. EPPLER 852