1–20 von 9,852 Ergebnissen
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    Zone-Based Modeling Technique for Vulnerability/Lethality Studies

    Butkiewicz, Mark / Bowman, W. | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Zinc Oxide Nanowire Interphase for Enhanced Lightweight Polymer Fiber Composites

    Ehlert, Gregory / Sodano, Henry | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

    ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization

    Chen, P.C. / Zhang, Z / Livne, Eli | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Zero-v Cellular Honeycomb Flexible Skins for One-Dimensional Wing Morphing AIAA Paper 2007-1735 CD-ROM Number 8

    Olympio, K. / Gandhi, F. | British Library Conference Proceedings | 2007
    Schlagwörter: Structures , Structural dynamics , Materials

    Zero-v Cellular Honeycomb Flexible Skins for One-Dimensional Wing Morphing

    Olympio, Kingnide / Gandhi, Farhan | AIAA | 2007
    Verlag: The American Institute of Aeronautics and Astronautics

    Zero- and One-g Comparison of Ripple Amplitude in Single-Curved Parabolic Membranes Using Photogrammetry

    Meyer, Christopher / Leifer, Jack / Lopez, Bernardo et al. | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    X-HALE: A Very Flexible UAV for Nonlinear Aeroelastic Tests

    Cesnik, Carlos / Senatore, Patrick / Su, Weihua et al. | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    XFEM Toolkit for Delamination Failure Prediction of Composite Bonded Pi Joints

    Lua, Jim / Flansburg, Barrett / Engelstad, Steve | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

      XFEM Toolkit for Delamination Failure Prediction of Composite Bonded Pi Joints

      Lua, J. / Flansburg, B. / Engelstad, S. | British Library Conference Proceedings | 2009
      Schlagwörter: Materials , Structural dynamics

    XFEM Toolkit for Crack Path and Life Prediction of Aluminum Structures

    Lua, Jim / Shi, Jay / Liu, Philip et al. | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

      XFEM Toolkit for Crack Path and Life Prediction of Aluminum Structures

      Lua, J. / Shi, J. / Liu, P. et al. | British Library Conference Proceedings | 2009
      Schlagwörter: Materials , Structural dynamics

    X-FEM Toolkit for Automated Crack Onset and Growth Prediction

    Shi, Jay / Lua, Jim / Waisman, Haim et al. | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    X-FEM for Three-Dimensional Dynamic Crack Growth

    Ni, Kan / Hu, Patrick / Fan, Xiaochen et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    X-FEM Co-Simulation of Delamination and Matrix Cracking in Fiber Metal Laminated Structures under Fatigue Loading

    Fang, Eugene / Stuebner, Michael / Lua, Jim | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

      X-FEM Co-Simulation of Delamination and Matrix Cracking in Fiber Metal Laminated Structures under Fatigue Loading

      Fang, E. / Stuebner, M. / Lua, J. et al. | British Library Conference Proceedings | 2013
      Schlagwörter: Structural dynamics

    X-34 Dynamic Modeling and Correlation

    Blades, E. / Blelloch, P. / Dragone, T. et al. | British Library Conference Proceedings | 2000
    Schlagwörter: structural dynamics

    X33 Transient Liftoff Analysis

    Brunty, J. A. / Peck, J. A. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000
    Schlagwörter: structural dynamics

    X-33/RLV System Health Management/Vehicle Health Management

    Garbos, Raymond / Mouyos, William | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    X-33/RLV Reusable Cryogenic Tank VHM using fiber optic distributed sensing technology

    Bodan, Patricia / Bouvier, Carl | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    X-32 Aeroservoelasticity

    Hunziker, Scott | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    X-31A flight flutter test excitation by control surfaces

    Hodson, C.H. / Dobbs, S.K. / Brosman, M.J. et al. | Tema Archiv | 1993
    frequencies and damping versus dynamic pressure and mach number extracted from the response data are given. The required structural modes were ...

    Wrinkling of Orthotropic Viscoelastic Membranes

    Deng, Xiaowei / Pellegrino, Sergio | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Wrinkling of an Inflated Membrane with Thermo-Elastic Boundary Restraint

    Fitzgerald, D. / Jenkins, C. / Liu, X. et al. | British Library Conference Proceedings | 2000
    Schlagwörter: structural dynamics