Similarly shaped airfoils to EPPLER 560
New! Bulk download of polars in Excel format: e560.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. GOE 626
3. EPPLER 561
4. Joukowsky 16.00% thick 5.00% camber
5. Joukowsky 15.00% thick 5.00% camber
6. GOE 567
7. EPPLER 399
8. EPPLER 793
9. Joukowsky 17.00% thick 5.00% camber
10. NM Retro 16
11. MS535-1
12. GOE 413
13. EPPLER 562
14. MID 403
15. GOE 433
16. GOE 498
17. Joukowsky 16.00% thick 6.00% camber
18. GOE 612
19. GOE 621
20. Joukowsky 14.00% thick 5.00% camber
21. Joukowsky 15.00% thick 6.00% camber