LIBROS DEL AUTOR: brandon j adams

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  • Structural Stability of a Joined-Wing Sensorcraft
    Brandon J. Adams
    This thesis employed a multi-disciplinary design approach to determine the structural stability of the Boeing Joined-Wing SensorCraft. Specifically, this thesis sought to characterize the free vibration modes, ensure a buckling safe design and determine the influence of the geometric and aeroelastic nonlinearities associated with this joined-wing design. The clamped-free vibrat...
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