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Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter

EngineeringAeroelastic ParametersAerospace EngineeringAerospace SimulationFluid MechanicsMechanical EngineeringF-16 FighterAeroelasticityStructure InteractionAerodynamicsAerospace Propulsion Systems