Similarly shaped airfoils to EPPLER 344
New! Bulk download of polars in Excel format: e344.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. NACA45014.5
3. Fraser_f4fras15
4. NACA45014
5. FX 77-W-153
6. USA 45
7. GOE 632
8. Eiffel 371 (Monge)
9. NACA45013.5
10. DEFIANT CANARD BL110
11. NACA64-715 a=0.0
12. NACA63-715 a=0.0
13. EPPLER 338
14. NACA64-715 a=0.2
15. EPPLER 329
16. NACA65-715 a=0.0
17. NACA63-715 a=0.2
18. NACA64-716 a=0.0
19. NACA63-716 a=0.0
20. NACA64-615 a=0.2
21. NACA63-615 a=0.2