Now showing items 1-1 of 1
Characterisation of wind tunnel observed, large-amplitude pitch limit-cycles
(American Institute of Aeronautics and Astronautics, AIAA, 2011-09)
A five-degree-of-freedom dynamic wind tunnel rig is used in the observation of large amplitude self-sustaining pitch oscillations of a model aircraft. These oscillations arise during a quasi-steady ramp input to the aircraft ...