Approximate relations and charts for low-speed stability derivatives of swept wings

Thomas A. Toll, M. J. Queijo
naca-tn-1581
May 1948


A simplified theory has been used to drive approximate relations for the low-speed stability derivatives of swept wings. The analysis is made only for wings without dihedral, but the effects of sweep angle, aspect ratio, center-of-gravity location, and, in most instances, taper ratio are considered.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1948/naca-tn-1581.pdf