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

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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 ventilation suspended. https://cosmeticssquadets.shop/product-category/hand-wash/
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