1–20 von 86 Ergebnissen
|

    42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference : 16 - 19 April 2001, Seattle, Washington

    Structures, Structural Dynamics and Materials Conference and Exhibit / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers et al. | TIBKAT | 2001
    Verlag: American Inst. of Aeronautics and Astronautics , Reston, Va.

    39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference : April 20 - 23, 1998, Long Beach, CA

    Structures, Structural Dynamics and Materials Conference / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers et al. | TIBKAT | 1998
    Verlag: American Inst. of Aeronautics and Astronautics , Reston, Va.

    Structural Dynamics Analysis and Model Validation of Wind Turbine Structures

    Griffith, D. | British Library Conference Proceedings | 2009
    Schlagwörter: Materials , Structural dynamics

    Materials and Innovations for Large Blade Structures: Research Opportunities in WInd Energy Technology

    Ashwill, T. | British Library Conference Proceedings | 2009
    Schlagwörter: Materials , Structural dynamics

    Defect-Tolerant Structural Design of Wind Turbine Blades

    Wetzel, K. | British Library Conference Proceedings | 2009
    Schlagwörter: Materials , Structural dynamics

    Composite material compatibility with liquid and gaseous oxygen

    Robinson, M.J. / Stoltzfus, J.M. / Owens, T.N. | Tema Archiv | 2001
    Boeing and NASA are investigating the compatibility of composite materials with liquid and gaseous oxygen (LOX and GOX). The objective is ...

    Development of coilable longerons using Elastic Memory Composite material

    Lake, M.S. / Hazelton, C.S. / Murphey, T.W. et al. | Tema Archiv | 2002
    application to deployable space structures that rely on stored strain energy for deployment. The key difference between EMC materials and traditional ...

    The fundamentals of designing deployable structures with Elastic Memory Composites

    Lake, M.S. / Beavers, F.L. | Tema Archiv | 2002
    Elastic Memory Composite (EMC) materials exhibit many favorable qualities for deployable space structures and have piqued a broad interest ...

    Structural stability of a stiffened aluminum fuselage panel subjected to combined mechanical and internal pressure loads

    Rouse, M. / Young Richard D. / Gehrki, R.E. | Tema Archiv | 2003
    Results from an experimental and analytical study of a curved stiffened aluminum panel subjected to combined mechanical and internal ...

    Electrically conductive materials for thermal isolation in spacecraft charging environments

    Erikson, R. | Tema Archiv | 2001
    conductivity is reviewed, with theoretical and practical material options. Extremely thin titanium sandwich construction, carbon-loaded fiberglass ...

    Using a genetic algorithm for structural topology design of helicopter rotor blades

    Fanjoy, D.W. / Crossley, W.A. | Tema Archiv | 2001
    Topology design methods are useful tools for conceptual design of structural components because they can be used to represent nearly any ...

    On the use of component modes in multibody dynamics

    Craig, R.R. jun. / Anthony, T.C. | Tema Archiv | 1996
    characterize the elastic deformation of the articulating component. Analysis of the dynamics of spacecraft with articulating appendages, robots, and ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston
    Schlagwörter: Dynamik

    Semiactive vibration suppression of truss structures by ER fluid damper

    Onoda, J. / Oh, H.U. / Minesugi, K. | Tema Archiv | 1996
    To semiactively suppress the vibration of space truss structures, a variable damper using Electro-Rheological (ER) fluid is designed and ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    Structural analysis of a flexible structural member protruding into an interior flow field

    Weaver, M.A. / Gramoll, K.C. / Roach, R.L. | Tema Archiv | 1993
    element structural model, and a finite difference flow model form the basis of the solution method. The structure is iteratively loaded, with load ...

    A revolute joint with linear load-displacement response for precision deployable structures

    Lake, M.S. / Warren, P.A. / Peterson, L.D. | Tema Archiv | 1996
    NASA Langley Research Center is developing key structures and mechanisms technologies for micron-accuracy, in-space deployment of future ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    ASTROS for reliability-based multidisciplinary structural analysis and optimization

    Luo, Xiaodong / Grandhi, R.V. | Tema Archiv | 1995
    In conducting multidisciplinary structural optimization, there is uncertainty and randomness in he input information of finite element ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Washington

    Optimization of Aircraft Wings Including Dynamic Aeroelasticity and Manufacturing Aspects

    Petersson, O. | British Library Conference Proceedings | 2009
    Schlagwörter: Materials , Structural dynamics

    Structural system reliability under multiple failure modes

    Mahadevan, S. / Chamis, C.C. | Tema Archiv | 1993
    This paper describes a computational method for system reliability estimation of propulsion structures. The failure domain of the entire ...

    Advanced main combustion chamber structural jacket strength analysis

    Johnston, L.M. / Perkins, L.A. / Price, J.M. et al. | Tema Archiv | 1993
    The structural analysis of the Advanced Main Combustion Chamber (AMCC) is presented. The AMCC is an advanced fabrication concept of the ...