On unsteady aerodynamic airfoil loads in the design of a control system for minimizing the effect of wind perturbations using the rudder on the trailing edge of the wing.l

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dc.contributor.author Goman, M. (Mikhail G.) en
dc.contributor.author Sidoryuk, M. E. (Maria E.) en
dc.contributor.author Khrabrov, A. N. (Alexander N.) en
dc.date.accessioned 2008-11-24T14:10:10Z
dc.date.available 2008-11-24T14:10:10Z
dc.date.issued 2006-01-01 en
dc.identifier.citation Goman, M.G., Sidoryuk, M.E. and Khabrov, A.N. (2006) On unsteady aerodynamic airfoil loads in the design of a control system for minimizing the effect of wind perturbations using the rudder on the trailing edge of the wing. Journal of Computer and Systems Sciences International, 45(5), pp. 812-823.
dc.identifier.issn 1064-2307 en
dc.identifier.issn 1555-6530
dc.identifier.uri http://hdl.handle.net/2086/322
dc.description An output from research collaboration with TsAGI, Russia resulting in a revision of unsteady aerodynamics representation in active control alleviation of wind gust loads. The project was funded by ONERA, France in support of experimental tests on the free flight catapult facility in ONERA-Lille, designed for evaluation of unsteady aerodynamic effects during penetration of aircraft scaled model in the short gust (TsAGI Deputy Director V.L. Soukhanov, flight15@tsagi.ru). en
dc.language.iso en en
dc.publisher SpringerLink en
dc.subject RAE 2008
dc.subject UoA 28 Mechanical, Aeronautical and Manufacturing Engineering
dc.title On unsteady aerodynamic airfoil loads in the design of a control system for minimizing the effect of wind perturbations using the rudder on the trailing edge of the wing.l en
dc.type Article en
dc.identifier.doi http://dx.doi.org/10.1134/S1064230706050121 en
dc.researchgroup Centre for Engineering Science and Advanced Systems


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