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    Active and passive vibration control of a satellite during lift-off

    Lee-Glauser, G.J. / Ahmadi, G. / Layton, J.B. | Tema Archive | 1995
    rubber bearing and resilient friction systems are considered. Effectiveness of different vibration control systems for protection of the Space ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Aeroelastic stability analysis of an airfoil with structural nonlinearities using a state space unsteady aerodynamics model

    Murty, H.S. | Tema Archive | 1995
    airfoil. This analysis was carried out using a state space formulation for the aerodynamic model. This formulation enables hard coupling between ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    An enhanced analysis method for composite overwrapped pressure vessels

    Shu, J.C. / Chiu, S.T. / Chang, J.B. | Tema Archive | 1995
    The increasing use of composite overwrapped pressure vessels (COPVs) in space applications demands a comprehensive and reliable analysis ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    A new substructures system identification method

    Craig, R.R. jun. | Tema Archive | 1995
    A new method is proposed for system identification of substructures, such as payloads to be flown aboard the Space Shuttle. In the ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    A physical explanation of free play effects on the flutter response of an all movable control surface

    Pitt, D.M. | Tema Archive | 1995
    Aicraft Modeling Using State Space', (FAMUSS), computer code was used to generate state models at selected velocities. Two different state models ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Closed-loop vibration control experiments on a rotor with blade mounted actuation

    Prechtl, E.F. / Hall, S.R. | Tema Archive | 2000
    A Mach-scaled CH-47 model rotor blade with an actively controlled servo-flap near the tip was designed, manufactured, and tested. The servo ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Configuration-shape-size optimization of space structures using the webbing approach

    Vandenbelt, D.N. / Felippa, C.A. | Tema Archive | 1995
    This project investigates the configuration-shape-size optimization (CSSO) of orbiting and planetary space structures. The CSSO problem has ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Corrosion prediction in aging aircraft materials using neural networks

    Bailey, R.A. / Pidaparti, R.M. / Jayanti, S. et al. | Tema Archive | 2000
    exposed to two corrosive environments. Given the corrosion environment and time of exposure the first neural network predicts the ASTM G34 ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Damage tolerance of cracked cylindrical shells under internal pressure

    Hoogkamer, D. / Waas, A.M. / Arbocz, J. | Tema Archive | 2000
    centralized cracks at angles to the shell generators ranging from 0 degree to 90 degree at an interval of 15 degree and of various crack length, are ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Damage tolerance of fiber composite airfoils with piezoelectric adaptive control system

    Minnetyan, L. / Chamis, C.C. / Abdi, F. | Tema Archive | 2000
    . Progressive damage and fracture of a laminated composite airfoil subjected to external pressure loading and adaptive control stresses is evaluated via ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

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