Similarly shaped airfoils to EPPLER 332
New! Bulk download of polars in Excel format: e332.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. NACA34012
4. HS 3.4.12b
5. EPPLER 637
6. NACA35012
7. Horten 11.00% thick 3.00% camber
8. HS 3.5/12
9. EPPLER 331
10. Horten 12.00% thick 3.00% camber
11. Horten 11.00% thick 4.00% camber
12. Horten 12.00% thick 4.00% camber
13. NACA34112
14. NACA34010.5
15. NACA44012
16. NACA34110.5
17. EPPLER 635
18. NACA35010.5
19. BOEING-VERTOL VR-12
20. NACA35112
21. NACA25112