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dc.contributor.authorKhrabrov, A. N. (Alexander N.)en
dc.contributor.authorSidoryuk, M. E. (Maria E.)en
dc.contributor.authorGoman, M. (Mikhail G.)en
dc.date.accessioned2013-10-07T10:07:48Z
dc.date.available2013-10-07T10:07:48Z
dc.date.issued2013-06
dc.identifier.citationKhrabrov, A. N., Sidoryuk, M.E. and Goman, M. (2013) Aerodynamic model development and simulation of airliner spin for upset recovery. Progress in Flight Physics, 5, pp. 621 - 636.en
dc.identifier.urihttp://hdl.handle.net/2086/9104
dc.description.abstractThe aerodynamic model of a generic airliner configuration is developed for a wide range of angles of attack, sideslip and angular rate based on experimental data obtained in wind tunnels using static, forced oscillations and rotary balance tests. The developed aerodynamic model is applied for the investigation of the airliner scaled model nonlinear dynamics at high angles of attack with an intensive rotation to identify potential spin modes and spin recovery procedures. The evaluated equilibrium spin parameters and simulated recovery control deflections are in good agreement with the experimental results from free-spin tests obtained in the TsAGI vertical wind tunnel. The work is performed in connection with the European FP7 project SUPRA (Simulation of UPset Recovery in Aviation, www.supra.aero).en
dc.language.isoenen
dc.publisherEDP Sciencesen
dc.titleAerodynamic model development and simulation of airliner spin for upset recoveryen
dc.typeArticleen
dc.identifier.doihttp://dx.doi.org/10.1051/eucass/201305621
dc.researchgroupCentre for Engineering Science and Advanced Systemsen
dc.peerreviewedYesen
dc.funderECen
dc.projectidSUPRAen


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