Joukowsky 13.00% thick 4.00% camber


New! Bulk download of polars in Excel format: Joukowsky%2013.00%25%20thick%204.00%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
5Joukowsky 13.00% thick 4.00% camberFLAP5C35
15Joukowsky 13.00% thick 4.00% camberFLAP15C35
25Joukowsky 13.00% thick 4.00% camberFLAP25C35
35Joukowsky 13.00% thick 4.00% camberFLAP35C35
45Joukowsky 13.00% thick 4.00% camberFLAP45C35
-5Joukowsky 13.00% thick 4.00% camberFLAPM5C35
-15Joukowsky 13.00% thick 4.00% camberFLAPM15C35
-25Joukowsky 13.00% thick 4.00% camberFLAPM25C35
-35Joukowsky 13.00% thick 4.00% camberFLAPM35C35
-45Joukowsky 13.00% thick 4.00% camberFLAPM45C35