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Experimental Analysis of High Reynolds Number Aero-Structural Dynamics in ETW
The paper reports about the aero-structural dynamical experiments with an elastic wing model which were conducted during the High Reynolds Number Aero-Structural Dynamics project by RWTH AachenExpand
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Dynamic qualification of the HIRENASD elastic wing model
Abstract The High Reynolds Number Aero-Structural Dynamics (HIRENASD) project is conducted by the Collaborative Research Center “Flow Modulation and Fluid-Structure Interaction at Airplane Wings (SFBExpand
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HIGH REYNOLDS NUMBER AEROSTRUCTURAL DYNAMICS EXPERIMENTS IN THE EUROPEAN TRANSONIC WINDTUNNEL ( ETW )
The paper gives an overview of an experimental high Reynolds number aerostructural dynamics project with forthcoming experiments in the European Transonic Windtunnel. Starting with the generalExpand
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Aero-structural Dynamics Experiments at High Reynolds Numbers
The elastic wing model, its excitation and comprehensive high frequency measuring equipment for the High Reynolds Number Aero-Structural Dynamics (HIRENASD) tests in the European Transonic WindtunnelExpand
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Design, Qualification and Experimental Investigation on Flexible Wind Tunnel Wing Models
The purpose of this work on highly flexible wing models is the validation of the numerical direct simulation, developed in the Collaborative Research Center SFB 401. The first step in the validationExpand
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