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    Dynamic Simulation and Hydro-elastic Stability Analysis of Flexible Supercavitating Projectiles

    , Ph.D. Dissertation Sharif University of Technology Ahmadi Tehrani, Majid (Author) ; Dehghani Firouzabadi, Roohallah (Supervisor)
    Abstract
    At high speeds, cavitation bubbles form at the sharp edges of the submerged body or in situations where the pressure falls below the fluid vapor pressure. By placing a suitable cavitator in the nose of the body, the cavitation bubbles are cobined by increasing the speed and the whole body is placed inside the cavity. The formation of a supercavity leads to a significant reduction in the drag force of the vehicle. The submersible device is in contact with the fluid at two points, the cavitator and the fins, and due to the location of the cavitator in the nose of the body, the forces acting on it play an important role in the stability and control of the device.The main goal of current... 

    Development of the Hale Aircraft's Aeroelastic Model with Very Flexible Wings

    , Ph.D. Dissertation Sharif University of Technology Borhanpanah, Mohammad Reza (Author) ; Dehghani Firouzabadi, Roohallah (Supervisor)
    Abstract
    In this study, a nonlinear aeroelastic model for an aircraft with fully flexible wings is obtained. This aeroelastic model is based on system identification and is created using the beam model for the structure and the three-dimensional panel method for aerodynamic analysis. The model intended for the structure is a nonlinear beam with exact geometry with initial deformation and rigid motion. The model intended for aerodynamics is an unsteady three-dimensional panel method for the airplane’s body, wings, and tail. The desired aeroelasticity model is a reduced-order model based on system identification using the time-domain/frequency-domain aerodynamic response under forced vibrations in the...