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. M-35A-12.7
7. Horten 12.00% thick 3.00% camber
8. EPPLER 637
9. NACA34012
10. Horten 11.00% thick 3.00% camber
11. HS 3.5/12
12. HS 3.4.12b
13. EPPLER 635
14. NACA35012
15. EPPLER 331
16. NACA34110.5
17. NACA35112
18. NACA44012
19. NACA34010.5
20. MH 80 12.72%
21. NACA44112