Similarly shaped airfoils to EPPLER 852
New! Bulk download of polars in Excel format: e852.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. NACA63A410
3. NACA65-510
4. NACA64A410
5. NACA63-510
6. NACA64-410 a=0.8
7. NACA65-410 a=0.8
8. NACA63-410 a=0.8
9. YS-930
10. EPPLER 212
11. EM J8 2510 DrW
12. EPPLER 222
13. NACA64-511
14. EPPLER 211
15. NACA65A410
16. NACA63-511
17. HN-1023
18. NACA64-411 a=0.8
19. EM J18 2310
20. HQ 2.5/10
21. AH21 7% version