Similarly shaped airfoils to EPPLER 329
New! Bulk download of polars in Excel format: e329.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
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2. NACA45013.5
3. FX 63-143
4. NACA45014
5. NACA45013
6. HL80-133
7. EPPLER 343
8. ONERA OA213
9. NACA35013.5
10. EPPLER 342
11. NACA35013
12. NACA35014
13. NACA64-614 a=0.0
14. NACA45014.5
15. NACA63-614 a=0.0
16. NACA65-614 a=0.0
17. NACA64-514 a=0.2
18. Eiffel 371 (Monge)
19. NACA63-514 a=0.2
20. NACA65-514 a=0.2
21. HS 3.4.12b