NACA4416
NACA4416
New! Bulk download of polars in Excel format: NACA4416.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (9) | 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:
Panstwowe Zaklady Lotnicze PZL Mielec M-18A Dromader wing root
Panstwowe Zaklady Lotnicze PZL Mielec M-24 Super Dromader wing root
Schweizer SGS 2-12 TG-3A wing root
Schweizer SGS 2-12 TG-3A wing tip
Shield Xyla wing tip
Slingsby T.12 Kirby Gull 1 wing root
Slingsby T.14 Gull wing root
Slingsby T.15 Gull wing root
Slingsby T.25 Gull wing root