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title: aiaa space and astronautics form and exposition

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    Space program supporting technologies: structures, materials, and signal processing

    Schutzenhofer, L.A. / Blalock, S.J. / Johnston, L. et al. | Tema Archive | 1995
    task provides a benefit that addresses a problem area or meets a need in a space program. These benefits and past application of existing ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Space Shuttle Orbiter landing loads optimization

    Purtle, L.V. / Fann, C.P. / Eich, P.G. | Tema Archive | 1995
    The paper discusses the method used in the Space Shuttle program to optimize landing gear loads and requirements to support increased ...
    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

    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

    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

    Reduced-order modeling for flutter prediction

    Pettit, C.L. / Beran, P.S. | Tema Archive | 2000
    proper orthogonal decomposition technique. The flow is assumed to be inviscid and is modeled with the Euler equations. These nonlinear equations ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Dynamic Finite Element (DFE) formulation for coupled flap-lag vibrations of propeller blades

    Hashemi, S.M. / Golnaraghi, M.F. | Tema Archive | 2000
    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

    Probabilistic analysis of docking mechanism-induced loads for mir/shuttle mission

    Lin, H.Z. / Ghofranian, S. / Schmidt, M. et al. | Tema Archive | 1995
    This paper presents a methodology for probabilistic loads analysis and its application to the STS-71 orbiter/Mir space station docking. It ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Simulation of Shuttle/Mir docking

    Ghofranian, S. / Schmidt, M.S. / Schliesing, J. et al. | Tema Archive | 1995
    This paper describes the simulation of the docking system of the Space Shuttle orbiter and the Russian space station Mir. The system is a ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Washington

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