Similarly shaped airfoils to EPPLER 435
New! Bulk download of polars in Excel format: e435.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. FX 73-K-170/22
3. FX 73-170
4. EPPLER 657
5. NACA65-716 a=0.8
6. EPPLER 580
7. FX 62-K-153/20
8. NACA64A716
9. NACA63A716
10. NLF-1015
11. EPPLER 656
12. NACA64-716 a=0.8
13. NACA65-717 a=0.8
14. Dees Okay230
15. EPPLER 431
16. NACA64-717 a=0.8
17. EPPLER 432
18. EPPLER 654
19. NACA63-716 a=0.8
20. EPPLER 678
21. NACA63-717 a=0.8