81–100 von 275 Ergebnissen
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    Parametric Study of Joined-Wing Aircraft Geometry

    Sotoudeh, Zahra / Hodges, Dewey | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    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

    Aero-Acoustic Optimization of Airfoils for Wind Turbines

    Coimbra, Jaime F. / Marta, Andre C. | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

    Design for Flight Test of a Scaled Joined Wing SensorCraft

    Aarons, Tyler / Canfield, Robert / Woolsey, Craig et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Passive Load Control for Large Wind Turbines

    Ashwill, Tom | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Thermal structures - Four decades of progress

    Thornton, Earl A. | NTRS | 1990
    Since the first supersonic flight in October 1947, the United States has designed, developed and flown flight vehicles within increasingly ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Long-Term Loads and Motions for a Spar Buoy-Supported Floating Offshore Wind Turbine

    Manuel, Lance / Sultania, Abhinav | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Panel Resonant Behavior of Wind Turbine Blades

    Griffith, D. Todd / Paquette, Joshua | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Deflection-Based Structural Loads Estimation From the Active Aeroelastic Wing F/A-18 Aircraft

    Lizotte, Andrew M. / Lokos, William A. | NTRS | 2005
    using a reliable strain and structural deformation measurement system. The objective of this study was to explore the utility of a deflection ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Aircraft Design, Testing And Performance

    Analytical Approach for Estimating Preliminary Mass of ARES I Crew Launch Vehicle Upper Stage Structural Components

    Aggarwal, Pravin | NTRS | 2007
    system, Reaction Control System (RCS) for both the Upper Stage and the First Stage. MSFC's Spacecraft and Vehicle Department, Structural and ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Launch Vehicles And Launch Operations

    Embedded Sensors for Composite Wind Turbine Blades

    Cairns, Douglas / Palmer, Nathan / Ehresman, Jonathan | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Nonlinear Aeroelastic Studies on a Joined-Wing with Wing Buckling Effects

    Lee, Dong-Hwan / Chen, P. C. | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    Non-Deterministic Thermo-Fluid Analysis of a Compressor Rotor-Stator Cavity

    Gopinathrao, Naveen Prasad / Mabilat, Christophe / Alizadeh, Sohail | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

    Developing the Next Generation Shell Buckling Design Factors and Technologies

    Hilburger, Mark W. | NTRS | 2012
    NASA s Shell Buckling Knockdown Factor (SBKF) Project was established in the spring of 2007 by the NASA Engineering and Safety Center (NESC ...
    Verlag: NASA National Aeronautics and Space Administration
    Schlagwörter: Structural Mechanics

    A Model to Compare the Flight Control Energy Requirements of Morphing and Conventionally Actuated Wings

    Johnston, Christopher / Neal, David / Wiggins, Leonard et al. | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    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 ...

    Optimization of Aircraft Wings Including Dynamic Aeroelasticity and Manufacturing Aspects

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

    Development of Solar-Powered Aircraft for Multipurpose Application

    Rehman Alvi, Obaid | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Low Cost Inspection for Improved Wind Turbine Blade Reliability

    Cairns, Douglas / Palmer, Nathan / Ehresman, John | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

      Low Cost Inspection for Improved Wind Turbine Blade Reliability

      Cairns, D. / Palmer, N. / Ehresman, J. | British Library Conference Proceedings | 2009
      Schlagwörter: Materials , Structural dynamics

    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 ...