Similarly shaped airfoils to EPPLER 557
New! Bulk download of polars in Excel format: e557.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. EM J18 1 3015
3. NACA63(2)-615
4. NACA63-716
5. NACA63-715
6. EM J18 3015 DrW r0,8
7. NACA63-616 a=0.8
8. NACA63-615 a=0.8
9. NACA64-716
10. NACA64-715
11. EPPLER 562
12. FX 60-160
13. FX 75-141
14. FX 83-W-160
15. FX 61-147
16. GOE 493
17. Joukowsky 16.00% thick 4.00% camber
18. NACA64-616 a=0.8
19. EPPLER 580
20. NACA64-615 a=0.8
21. HQ 3.0/15