Similarly shaped airfoils to EPPLER 392
New! Bulk download of polars in Excel format: e392.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. PSU 94-097 (AIAA 2001-2478)
3. MH 116 9.84%
4. S4062-095-87
5. S2091-101-83
6. DAE-51
7. SD7034
8. GOE 602 MOD.
9. MH 38 9.68%
10. GA 35-610
11. NACA63-610 a=0.6
12. SD7043 (9.1%)
13. HQ 3.5/10
14. GA 37-610
15. GOE 389
16. NACA64-610 a=0.6
17. NACA63-610 a=0.8
18. GA 30-610
19. NACA63-610 a=0.5
20. GOE 596
21. GA 35A610