Similarly shaped airfoils to EPPLER 385


New! Bulk download of polars in Excel format: e385.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
Dynamic plotter New!
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.

1. GOE 118 (MVA MK.7)
2. GOE 610-B MOD.
3. NACA6409
4. GOE 195
5. HL73-650
6. GOE 456
7. GOE 458
8. Eiffel 36
9. Joukowsky 9.00% thick 6.00% camber
10. GOE 124 (MVA H.4)
11. GOE 428
12. GOE 439
13. GOE 450
14. GOE 174 (ALBATROS 5020)
15. GOE 359
16. Joukowsky 9.00% thick 5.00% camber
17. GOE 184 (MVA H.29)
18. GOE 176 (ALBATROS 7020)
19. GOE 610 B
20. AH-6-40-7
21. NACA63-709 a=0.6