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dc.contributor.authorAraujo-Estrada, Sergio A.en
dc.contributor.authorLowenberg, M. H.en
dc.contributor.authorNeild, Simonen
dc.contributor.authorGoman, M. (Mikhail G.)en
dc.date.accessioned2016-04-04T09:12:56Z
dc.date.available2016-04-04T09:12:56Z
dc.date.issued2015-01
dc.identifier.citationAraujo-Estrada, S.A., Lowenberg, M.H., Neild, S. and Goman, M. (2015) Evaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rig. AIAA Atmospheric Flight Mechanics Conference, AIAA SciTech, (AIAA 2015-0750).en
dc.identifier.urihttp://hdl.handle.net/2086/11792
dc.description.abstractThis paper discusses the development of a novel multi-degree-of-freedom dynamic manoeuvre rig aimed at investigation of aircraft upset/LOC-related behaviour in the wind tunnel. The motivation behind the development and characteristics of the rig are first described, along with example behaviour of an aircraft model exhibiting nonlinear time-dependent aerodynamics in an open-jet low-speed wind tunnel. Test objectives for assessment of upset onset scenarios - both for parameter estimation purposes and to 'physiccally simulate' the behaviour - are then described, as is the design of the upgraded instrumentation system to facilitate experimental investigation. Finally, examples of relevant behaviour involving real-time control of the rig to explore nonlinear conditions leading to upset are presented; these are evaluated in terms of prospects for such testing in aircraft development and analysis projects.en
dc.language.isoenen
dc.publisherAIAA Atmospheric Flight Mechanics Conferenceen
dc.titleEvaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rigen
dc.title.alternativeAIAA 2015-0750en
dc.typeConferenceen
dc.identifier.doihttp://dx.doi.org/10.2514/6.2015-0750
dc.researchgroupCentre for Engineering Science and Advanced Systemsen
dc.peerreviewedYesen
dc.funderN/Aen
dc.projectidN/Aen
dc.cclicenceN/Aen
dc.date.acceptance2015-01-08en


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