1–50 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

    Wrinkling and Gravity Effects on Transverse Vibration of Membranes

    Hossain, Awlad / Jenkins, Christopher / Woo, Kyeongsik et al. | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Wrinkling Analysis Using Improved Dynamic Relaxation Method AIAA Paper 2007-2350 CD-ROM Number 8

    Kashiwa, M. / Onoda, J. | British Library Conference Proceedings | 2007
    Schlagwörter: Structures , Structural dynamics , Materials

    Wrinkling Analysis Using Improved Dynamic Relaxation Method

    Kashiwa, Munetaka / Onoda, Junjiro | AIAA | 2007
    Verlag: The American Institute of Aeronautics and Astronautics

    Wrinkling Analysis of a Kapton Square Membrane Under Tensile Loading

    Su, Xiaofeng / Abdi, Frank / Taleghani, Barmac et al. | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    Wrinkle/Slack Control Using Shape Memory Polymer Films for Large Membrane Structures

    Senba, Atsuhiko / Ogi, Yoshiro / Kogiso, Nozomu | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

      Wrinkle/Slack Control Using Shape Memory Polymer Films for Large Membrane Structures

      Senba, A. / Ogi, Y. / Kogiso, N. et al. | British Library Conference Proceedings | 2013
      Schlagwörter: Structural dynamics

    Wrinkle Generation Mechanism without Buckling in Sheared Rectangular Membrane

    Senda, Kei / Nakanishi, Kei / Takagi, Kazuya | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      Wrinkle Generation Mechanism without Buckling in Sheared Rectangular Membrane

      Senda, K. / Nakanishi, K. / Takagi, K. et al. | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Structures , Structural dynamics , Materials

    Wrinkle-Crease Interaction Simulation Using Combined MT Model and DP Technique

    Wang, Changguo / Tan, Huifeng / He, Xiaodong | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Wrinkle and Collapsing Process of Inflatable Tubes Under Bending Loads by Finite Element Analyses

    Furuya, Hiroshi / Yokoyama, Jin | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      Wrinkle and Collapsing Process of Inflatable Tubes Under Bending Loads by Finite Element Analyses

      Furuya, H. / Yokoyama, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Structures , Structural dynamics , Materials

    Wrapping and Through-Thickness Poisson Effects on Composite Plate and Shell Contact Laws

    Yamamoto, Namiko / Wicks, Nathan / Wardle, Brian | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Woven fabric composites - Developments in engineering bounds, homogenization and applications

    Chung, Peter / Tamma, Kumar | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    Worst Case Flutter Analysis of a Stored Wing with Structural and Aerodynamc Variation

    Chung, ChanHoon / Shin, SangJoon | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Wireless Smart -Tires for Road Friction Measurement and Self State Determination

    Palmer, Matthew / Boyd, Clark / McManus, Jim et al. | AIAA | 2002
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing Torsional Stiffness Tests of the Active Aeroelastic Wing F/A-18 Airplane

    Lokos, William / Olney, Candida / Crawford, Natalie et al. | AIAA | 2002
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing-Tail Interaction Flutter Revisited

    Yurkovich, R. / AIAA / ASME et al. | British Library Conference Proceedings | 1996
    Schlagwörter: structures , structural dynamics , materials

      Wing-tail interaction flutter revisited

      Yurkovich, R. | Tema Archiv | 1996
      . In this case the flap provides the downwash necessary for the aerodynamic coupling between the wing and the horizontal tail. In the earlier ...
      Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston
      Schlagwörter: Dynamik

    Wing Structural Optimization Using Adaptive Metamodels Based on Fuzzy Clustering

    Zhu, Huaguang / Liu, Li / Yang, W. et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing Mechanization Design and Analysis for a Perching Micro Air Vehicle

    Lukens, Jennifer / Reich, Gregory / Sanders, Brian | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing Line Discretization for the Development of a Modular Morphing Wing

    Finistauri, Allan / Xi, Fengfeng / Walsh, Paul et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Wing flutter boundary prediction using unsteady Euler aerodynamic method

    Lee-Rausch, E.M. / Batina, J.T. | Tema Archiv | 1993
    algorithm and the addition of the structural equations of motion for their simultaneous time-integration with the governing flow equations. The ...

    Wing design for a civil filt-rotor transport aircraft: A preliminary study

    Rais-Rohani, M. / Baker, D.J. | Tema Archiv | 1994
    to identify the proper procedures to analyze these characteristics; and to develop the structural modeling and analysis techniques necessary ...

    Wing Design as a Symphony of Geographically Dispersed, Multi-disciplinary Undergraduate Students

    Zender, Fabian / Schrage, Daniel / Richey, Michael et al. | AIAA | 2013
    Verlag: The American Institute of Aeronautics and Astronautics

      Wing Design as a Symphony of Geographically Dispersed, Multi-disciplinary Undergraduate Students

      Zender, F. / Schrage, D. / Richey, M. et al. | British Library Conference Proceedings | 2013
      Schlagwörter: Structural dynamics

    Wind Turbine Blade Structural Efficiency

    Buckney, Neil / Green, Steven / Pirrera, Alberto et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      Wind Turbine Blade Structural Efficiency

      Buckney, N. / Green, S. / Pirrera, A. et al. | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Structures , Structural dynamics , Materials

    Wind Tunnel to Atmospheric Mapping for Static Aeroelastic Scaling

    Heeg, Jennifer / Spain, Charles / Rivera, Jose | AIAA | 2004
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Tests to Modify a Drag-Type Vertical Axis Wind Turbine

    Vallone, William / Guven, Ibrahim / Madenci, Erdogan | AIAA | 2010
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Test of a Very Flexible Aircraft Wing

    Britt, Robert / Ortega, Daniel / Mc Tigue, John et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

      Wind Tunnel Test of a Very Flexible Aircraft Wing

      Britt, R. / Ortega, D. / McTigue, J. et al. | British Library Conference Proceedings | 2012
      Verlag: American Institute of Aeronautics and Astronautics , Reston, VA
      Schlagwörter: Structures , Structural dynamics , Materials

    Wind Tunnel Testing of a Twisted Wing for Longitudinal Control in a Joined-Wing Aircraft AIAA Paper 2007-1772 CD-ROM Number 8

    Bond, V. / Canfield, R. / Matos, M.M.S. et al. | British Library Conference Proceedings | 2007
    Schlagwörter: Structures , Structural dynamics , Materials

    Wind Tunnel Testing of a Twisted Wing for Longitudinal Control in a Joined-Wing Aircraft

    Bond, Vanessa / Canfield, Robert / Madruga Santos Matos, Maria da Luz et al. | AIAA | 2007
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Testing of an Active Controlled Wing Under Gust Excitation

    Ricci, Sergio / Scotti, Alessandro | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Testing of a Lightweight One-Quarter-Scale Actuator Utilizing Shape Memory Alloy

    Ruggeri, Robert / Arbogast, Darin / Bussom, Richard | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    Wind Tunnel Studies of Damaged-Wing Induced Limit Cycle Oscillations AIAA Paper 2007-1799 CD-ROM Number 8

    Park, H. / Kim, T. / Stearman, R. et al. | British Library Conference Proceedings | 2007
    Schlagwörter: Structures , Structural dynamics , Materials

    Wind Tunnel Studies of Damaged-Wing Induced Limit Cycle Oscillations

    Park, Hyeonsu / Kim, Taekhyun / Stearman, Ronald et al. | AIAA | 2007
    Verlag: The American Institute of Aeronautics and Astronautics