Wind tunnel tests on a model of a monoplane wing with floating ailerons

Montgomery Knight, Millard J. Bamber
naca-tn-316
Sep 1929


This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with wing tip floating ailerons. Lift and drag, as well as rolling and yawing moments, were measured.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1929/naca-tn-316.pdf