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
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).
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.
ISSN : 1064-2307
1555-6530
1555-6530
Research Group : Centre for Engineering Science and Advanced Systems