The unsteady lift of a wing of finite aspect ratio

Jones, Robert T
naca-report-681
1940


Unsteady-lift functions for wings of finite aspect ratio have been calculated by correcting the aerodynamic inertia and the angle of attack of the infinite wing. The calculations are based on the operational method.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1940/naca-report-681.pdf