Horten 11.00% thick 1.00% camber


New! Bulk download of polars in Excel format: Horten%2011.00%25%20thick%201.00%25%20camber.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
5Horten 11.00% thick 1.00% camberFLAP5C35
15Horten 11.00% thick 1.00% camberFLAP15C35
25Horten 11.00% thick 1.00% camberFLAP25C35
35Horten 11.00% thick 1.00% camberFLAP35C35
45Horten 11.00% thick 1.00% camberFLAP45C35
-5Horten 11.00% thick 1.00% camberFLAPM5C35
-15Horten 11.00% thick 1.00% camberFLAPM15C35
-25Horten 11.00% thick 1.00% camberFLAPM25C35
-35Horten 11.00% thick 1.00% camberFLAPM35C35
-45Horten 11.00% thick 1.00% camberFLAPM45C35