Similarly shaped airfoils to EPPLER 636
New! Bulk download of polars in Excel format: e636.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. EH 3.0/12
3. Horten 12.00% thick 4.00% camber
4. NACA34112
5. Horten 11.00% thick 4.00% camber
6. Horten 12.00% thick 3.00% camber
7. EPPLER 637
8. NACA34012
9. Horten 11.00% thick 3.00% camber
10. HS 3.5/12
11. HS 3.4.12b
12. EPPLER 635
13. NACA35012
14. EPPLER 331
15. NACA34110.5
16. NACA35112
17. NACA44012
18. NACA34010.5
19. MH 80 12.72%
20. NACA44112
21. NACA25112