Similarly shaped airfoils to EPPLER 562
New! Bulk download of polars in Excel format: e562.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. NM Retro 14
4. NM Retro 16
5. MID 403
6. GOE 650
7. MS535-2
8. EPPLER 210
9. Joukowsky 15.00% thick 4.00% camber
10. GS-1
11. MS535-1
12. Joukowsky 15.00% thick 5.00% camber
13. EPPLER 560
14. FX 63-145
15. NACA63-715 a=0.8
16. GOE 619
17. Joukowsky 14.00% thick 4.00% camber
18. EPPLER 557
19. NACA63-714 a=0.8
20. Joukowsky 16.00% thick 4.00% camber
21. USA 40