Computational framework for investigation of aircraft nonlinear dynamics.

De Montfort University Open Research Archive

Show simple item record Goman, M. (Mikhail G.) en Khramtsovsky, A. V. (Andrew V.) en 2008-11-24T14:10:10Z 2008-11-24T14:10:10Z 2007-05-21 en
dc.identifier.citation Goman, M.G. and Khramtsovsky, A.V. (2008) Computational framework for investigation of aircraft nonlinear dynamics. Advances in Engineering Software, 39(3), pp. 167-177.
dc.identifier.issn 0965-9978 en
dc.description A corrected proof of the paper available online since 24 May 2007. Output of collaboration between DMU, TsAGI, Russia and DERA/QinetiQ, UK in 1998-2004 (TsAGI Deputy Director Valeri Soukhanov, DERA/QinetiQ Technical Manager Yoge Patel The previous version of this software was acquired by ADA/India (Program Director T G Pai, DRA/UK. The software has been successfully applied and tested by shadowing QinetiQ flight clearance trials on weapons carriage on in-service aircraft in the UK: “…the results showed a high degree of correlation of off-line predictions of aircraft handling and performance with flight test data” (see AIAA-2003-5557 ). en
dc.description.abstract A computational framework based on qualitative theory, parameter continuation and bifurcation analysis is outlined and illustrated by a number of examples for inertia-coupled roll maneuvers. The focus is on the accumulation of computed results in a special database and its incorporation into the investigation process. Ways to automate the investigation of aircraft nonlinear dynamics are considered.
dc.language.iso en en
dc.publisher Elsevier en
dc.subject RAE 2008
dc.subject UoA 28 Mechanical, Aeronautical and Manufacturing Engineering
dc.title Computational framework for investigation of aircraft nonlinear dynamics. en
dc.type Article en
dc.identifier.doi en
dc.researchgroup Centre for Engineering Science and Advanced Systems

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