Similarly shaped airfoils to EPPLER 387
New! Bulk download of polars in Excel format: e387.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. SD6080 (9.2%)
3. NACA63-509 a=0.5
4. NACA63-509 a=0.6
5. EPPLER 176
6. NACA64-509 a=0.5
7. S4061-096-84
8. S3025 9.38%
9. MID 321a
10. NACA64-509 a=0.6
11. SA7038
12. MID 322
13. SB99 F3J
14. MID 321b
15. HOBIE SM
16. GOE 585
17. S4110
18. GA 35-410
19. NACA4409
20. NACA63-510 a=0.5
21. SA7036