Abstract:In a supersonic airflow, smart skin antenna structure is analyzed to investigate the thermo-mechanical characteristics and stability boundaries. The skin is modeled as a multi-layer sandwich structure with a dielectric polymer. Especially, the layer is embedded on the middle surface of the face sheets similar to the honeycomb core to perform the role of antenna or radar structures. First-order shear deformation theory of plate and von Karman strain-displacement relations are adopted in this work. Also, aerodyn… Show more
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