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dc.contributor.authorPattinson, J.en
dc.contributor.authorLowenberg, M. H.en
dc.contributor.authorGoman, M. (Mikhail G.)en
dc.date.accessioned2013-10-07T10:23:20Z
dc.date.available2013-10-07T10:23:20Z
dc.date.issued2011-09
dc.identifier.citationPattinson, J., Lowenberg, M. H. and Goman, M. (2011) Characterisation of wind tunnel observed, large-amplitude pitch limit-cycles. AIAA 2011-6526, AIAA Atmospheric Flight Mechanics Conference, 08-11 August 2011, Portland, Oregonen
dc.identifier.urihttp://hdl.handle.net/2086/9105
dc.description.abstractA 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 model’s elevator surfaces in one-degree-of-freedom pitch mode and in the longitudinal two-degree-of-freedom pitch and heave modes. A mathematical model of the aerodynamics, incorporating dynamic stall, is proposed. The model is coupled to the equations of motion of the rig, which include terms for friction, and fitted to the experimental data. This later process is achieved using continuation and bifurcation analysis and revealed the influence of friction forces on the oscillatory behavior. The quality of the fit and the use of a phenomenological model allows a possible cause for these oscillations to be proposed.en
dc.language.isoenen
dc.publisherAmerican Institute of Aeronautics and Astronautics, AIAAen
dc.titleCharacterisation of wind tunnel observed, large-amplitude pitch limit-cyclesen
dc.typeConferenceen
dc.identifier.doihttp://dx.doi.org/10.2514/6.2011-6526
dc.researchgroupCentre for Engineering Science and Advanced Systemsen
dc.peerreviewedYesen
dc.fundern/aen
dc.projectidn/aen


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