Similarly shaped airfoils to EPPLER 561
New! Bulk download of polars in Excel format: e561.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. GOE 433
3. GOE 626
4. Joukowsky 17.00% thick 5.00% camber
5. Joukowsky 16.00% thick 5.00% camber
6. GOE 498
7. GOE 413
8. EPPLER 559
9. Joukowsky 17.00% thick 6.00% camber
10. GOE 288
11. Joukowsky 16.00% thick 6.00% camber
12. Joukowsky 18.00% thick 5.00% camber
13. EPPLER 793
14. EPPLER 399
15. GOE 612
16. GOE 621
17. GOE 567
18. MS535-1
19. GOE 628
20. DOUGLAS LA203A
21. Joukowsky 15.00% thick 5.00% camber