Similarly shaped airfoils to EPPLER 1098
New! Bulk download of polars in Excel format: e1098.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. NACA64-619 a=0.8
3. NACA64-719
4. FX 66-S-196 V1
5. FX S 02-196
6. EPPLER 604
7. NACA64(3)-618
8. NACA65-719
9. NACA65-619 a=0.8
10. NACA64-719 a=0.8
11. NACA65-718
12. NACA65-618 a=0.8
13. FX 61-184
14. NACA63-619 a=0.8
15. HQ 3.5/18
16. NACA63-719
17. NACA64-618 a=0.8
18. NACA64-718
19. NACA63A618
20. NACA64A618
21. NACA63(3)-618