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Shape morphing of aircraft wing: Status and challenges

✍ Scribed by A.Y.N. Sofla; S.A. Meguid; K.T. Tan; W.K. Yeo

Publisher
Elsevier Science
Year
2010
Weight
498 KB
Volume
31
Category
Article
ISSN
0261-3069

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In this paper, we announce our recent results on the asymptotic and spectral analysis of the model of an aircraft wing in a subsonic air flow. This model has been developed in the Flight Systems Research Center of UCLA and is presented in the works by Balakrishnan. The model is governed by a system

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## Abstract The present paper is devoted to the asymptotic and spectral analysis of an aircraft wing model in a subsonic air flow. The model is governed by a system of two coupled integro‐differential equations and a two parameter family of boundary conditions modelling the action of the self‐strai