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

De Montfort University Open Research Archive

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

Goman, M. (Mikhail G.) ; Sidoryuk, M. E. (Maria E.) ; Khrabrov, A. N. (Alexander N.)
Subject: RAE 2008, UoA 28 Mechanical, Aeronautical and Manufacturing Engineering
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.

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).
URI: http://hdl.handle.net/2086/322
DOI: http://dx.doi.org/10.1134/S1064230706050121
ISBN: 1064-2307
1555-6530 (online)
Research Group: Centre for Engineering Science and Advanced Systems
Date: 2006-01-01

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