Abstract:This work presents energy harvesting from the limit cycle oscillation of low aspect ratio rectangular cantilever wings in supersonic ow. The wing is modeled according to the classical plate theory with von-Karman strain-displacement relations for modeling large de ections due to mid-plane stretching. The aerodynamic pressure is evaluated based on the quasi-steady rst-order piston theory. Linear and nonlinear aeroelastic characteristics of the considered model are accurately examined and the e ects of Ionic Pol… Show more
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