Similarly shaped airfoils to EPPLER 694
New! Bulk download of polars in Excel format: e694.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. NLF-1015
3. NACA66-716 a=0.8
4. NACA66-715 a=0.8
5. NACA65A716
6. NACA66A716
7. NACA66A715
8. EPPLER 662
9. EPPLER 587
10. EPPLER 435
11. NACA65A715
12. NACA67-715 a=0.8
13. FX 62-K-153/20
14. EPPLER 657
15. NACA67A715
16. EPPLER STE 87(-3)-914
17. NACA65-716 a=0.8
18. FX 73-170
19. NACA65A717
20. FX 73-K-170/22
21. NACA66-717 a=0.8