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    Orbiter tire traction and wear

    Michalopoulos, C.D. / Hamilton, D.A. | Tema Archive | 1995
    The traction and wear problem for a main landing gear tire of the Space Shuttle Orbiter is considered. Side force acting on the tire during ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Modeling of shock propagation and attenuation in viscoelastic materials

    Rusovici, R. / Lesieutre, G.A. / Inman, D.J. | Tema Archive | 2000
    address modeling of geometrically complex structures. These finite elements are then used to model shock propagation and absorption through ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Optimum design and testing of a post-buckled stiffened panel

    Lillico, M. / Butler, R. / Hunt, G.W. et al. | Tema Archive | 2000
    of an initial overall imperfection. The resulting panel has been analyzed using the non-linear FE package ABAQUS and four laboratory ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Energy based design and analysis of staggered solvers for nonlinear transient aeroelastic problems

    Pipeno, S. / Farhat, C. | Tema Archive | 2000
    partitioned procedure. We present a mathematical framework for assessing some important numerical properties of the chosen partitioned procedure, and ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Propagation and control of crack-like damage in curved composite panels under combined loads

    Mahler, M. / Ley, R. / Shah, C. et al. | Tema Archive | 2000
    Certification and damage tolerance criteria are critical technologies for the advancement of composites structures on commercial aircraft ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Design and experimental testing of an induced-shear piezoelectric actuator for rotor blade trailing edge flaps

    Centolanza, L.R. / Smith, E.C. | Tema Archive | 2000
    deflection and hinge moment. A finite element model of the actuator tube and trailing edge flap is used to compare the performance of the new tube ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    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

    Derivation of 0-g structural control models from analysis and 1-g experimentation

    Glaese, R.M. / Miller, D.W. | Tema Archive | 1995
    The Middeck Active Control Experiment (MACE) is a space shuttle flight experiment, manifest for launch on STS-67 on March 2, 1995, intended ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Fracture parameter evaluation of composite panels under in-plane loading

    Cai, G. / Yuan, F.G. | Tema Archive | 2000
    path once the failure criteria are reached. Fracture parameters such as stress intensity factor and T-stress are computed from the J-integral ...
    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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