NACA63-015
NACA63-015
New! Bulk download of polars in Excel format: NACA63-015.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (13) | 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.
Known applications:
Aviation Industries of Iran AVA-202 wing tip
Musger MG-23 wing root
Musger MG-23 wing tip
Cessna CH-1 Skyhook blade root
Cessna CH-1 Skyhook blade tip
Cessna YH-41 Seneca blade root
Cessna YH-41 Seneca blade tip
Fairchild Hiller FH-1100 blade root
Fairchild Hiller FH-1100 blade tip
Robinson R22 blade root
Robinson R22 blade tip
Robinson R44 blade root
Robinson R44 blade tip