Evaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rig

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dc.cclicenceN/Aen
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.acceptance2015-01-08en
dc.date.accessioned2016-04-04T09:12:56Z
dc.date.available2016-04-04T09:12:56Z
dc.date.issued2015-01
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.funderN/Aen
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.doihttps://doi.org/10.2514/6.2015-0750
dc.identifier.urihttp://hdl.handle.net/2086/11792
dc.language.isoenen
dc.peerreviewedYesen
dc.projectidN/Aen
dc.publisherAmerican Institute of Aeronautics and Astronauticsen
dc.researchgroupCentre for Engineering Science and Advanced Systemsen
dc.titleEvaluation of Aircraft Model Upset Behaviour Using Wind Tunnel Manoeuvre Rigen
dc.title.alternativeAIAA 2015-0750en
dc.typeConferenceen

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