HIGH-SPEED CONCURRENT TRANSMISSION SCHEME FOR FULL DUPLEX MULTI-HOP RELAY ASSISTED MMWAVE WPAN NETWORKS



Acquisition of Swept Aerodynamic Data by the Consecutive Changing of Wing Model Configuration in a Wind Tunnel Test Using Remote Feedback Control

This study conducted wind tunnel tests with consecutive deflection angle changes on a three-dimensional (3D) wing with a control surface to procure aerodynamic data by sweeping the deflection angle.Configuration changes of a wind tunnel test model, such as changing the deflection angle of control surfaces, are usually performed manually with the ve

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