Wind-tunnel investigation and analysis of the effects of end plates on the aerodynamic characteristics of an unswept wing

Donald R. Riley
naca-tn-2440
Aug 1951


A wind-tunnel investigation has been conducted to determine the effects of end plates of various areas and shapes on the aerodynamic characteristics of an unswept and untapered wing of aspect ratio 4.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-tn-2440.pdf