NACA63-415
NACA 63-415
New! Bulk download of polars in Excel format: NACA63-415.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (23) | 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:
Enaer Namcu wing root
Enaer Namcu wing tip
Euro-ENAER EE 10 Eaglet wing root
Euro-ENAER EE 10 Eaglet wing tip
FFA AS 202 Bravo wing tip
Korean Air Chang-Gong 91 wing root
Korean Air Chang-Gong 91 wing tip
PIK-19 wing root
PIK-19 wing tip
PIK-23 wing root
PIK-23 wing tip
Rockwell Commander 112 wing root
Rockwell Commander 112 wing tip
Rockwell Commander 114 wing root
Rockwell Commander 114 wing tip
SIAI-Marchetti SF.205 wing tip
SIAI-Marchetti SF.208 wing tip
Sikorsky S-72 RSRA wing root
Sikorsky S-72 RSRA wing tip
SSVOBB Impuls wing root
SSVOBB Impuls wing tip
Valmet Tuuli III wing tip
Valmet Tuuli IV wing tip