Experimental Validation of the Wing-Aileron-Tab Combination Applied to an Actively Controlled Bridge Section Model
نویسندگان
چکیده
Maria Boberg1,2, Glauco Feltrin1, Alcherio Martinoli2 1Structural Engineering Laboratory, Swiss Federal Laboratories for Materials Science and Technology, Duebendorf, Switzerland 2Distributed Intelligent Systems and Algorithms Laboratory, School of Architecture, Civil and Environmental Engineering, École Polytechnique Fédérale de Lausanne, Switzerland email: [email protected], [email protected], [email protected]
منابع مشابه
Ministry of Supply
This paper gives the results of an investigation into the effects of wing torsion in a ternary-type spring-tab flutter. The results presented are for a series of calculations on an idealised system having degrees of freedom in wing pitch, rotation of the control surface and rotation of the tab; the pitching degree of freedom is spring restrained and is intended to represent wing torsion. The ta...
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