Similarly shaped airfoils to EPPLER 558
New! Bulk download of polars in Excel format: e558.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 793
3. EPPLER 562
4. NM Retro 16
5. MS535-1
6. FX 66-S-161
7. Joukowsky 16.00% thick 4.00% camber
8. EPPLER 560
9. MID 403
10. Joukowsky 15.00% thick 4.00% camber
11. MID 415
12. GOE 413
13. EPPLER 557
14. FX 66-17A-175
15. EPPLER 580
16. GS-1
17. FX 66-S-171
18. Joukowsky 16.00% thick 5.00% camber
19. NACA63-715 a=0.8
20. GOE 619
21. NACA63-716 a=0.8