Similarly shaped airfoils to EPPLER 593
New! Bulk download of polars in Excel format: e593.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. EPPLER 598
3. FX 77-W-121
4. GOE 746
5. GOE 318 (HANSA-BRANDENBURG VI.5)
6. FAD21
7. GOE 323 (HANSA-BRANDENBURG V.1)
8. NACA63-710 a=0.0
9. GOE 316 (HANSA-BRANDENBURG IV.5)
10. NACA63-710 a=0.2
11. NACA63-711 a=0.0
12. NACA63-711 a=0.2
13. GOE 286
14. AQUILA 9.3% smoothed
15. NACA63-610 a=0.2
16. NACA45010
17. NACA64-710 a=0.0
18. NACA63-611 a=0.2
19. MILEY M06-13-128
20. NACA64-710 a=0.2
21. GOE 385