EM CY 1021 2010 X5 Fertig


New! Bulk download of polars in Excel format: EM%20CY%201021%202010%20X5%20Fertig.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
Dynamic plotter New!
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.


Angle (deg),
positive is trailing edge down
DAT File
5EM CY 1021 2010 X5 FertigFLAP5C35
15EM CY 1021 2010 X5 FertigFLAP15C35
25EM CY 1021 2010 X5 FertigFLAP25C35
35EM CY 1021 2010 X5 FertigFLAP35C35
45EM CY 1021 2010 X5 FertigFLAP45C35
-5EM CY 1021 2010 X5 FertigFLAPM5C35
-15EM CY 1021 2010 X5 FertigFLAPM15C35
-25EM CY 1021 2010 X5 FertigFLAPM25C35
-35EM CY 1021 2010 X5 FertigFLAPM35C35
-45EM CY 1021 2010 X5 FertigFLAPM45C35