1–50 of 1,434 hits
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    21st century steels for 21st customers: Flat and long steel product development

    Elliot, Chris | Tema Archive | 2007
    present day, the predominant structural solution is essentially the same, namely a fine high carbon-manganese steel pearlitic structure ...

    A Benchmark first-order shear-deformable triangular element for laminated composite structures

    Kosmatka, J. | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

    A building block approach to design verification testing of primary composite structure

    WHITEHEAD, R. / DEO, R. | AIAA | 1983
    Publisher: The American Institute of Aeronautics and Astronautics

    A cascade optmization strategy for solution of difficult multi-disciplinary design problems

    Patnaik, Surya / Coroneos, Rula / Hopkins, Dale et al. | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

    Accumulated damage and failure of finite-width composite laminates

    Johnson, Patrick / Chang, Fu-Kuo | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

    A Closed-Form Expression for Strain Energy Release Rate of Delamination

    Chan, W. S. / Kuo, W. J. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    A Combination of Immersed Methods and Compact Scheme Based Computational Fluid Dynamics for Fluid-Structure Interactions

    Wang, X. Sheldon / Gordnier, Raymond | AIAA | 2010
    Publisher: The American Institute of Aeronautics and Astronautics

    A Commerical Ready, High Reliable and High Producible RWA Design

    Fletcher, M. / Marshall, T. / Zuckerbrow, J. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    A comparison of optimization formulations for design minimization of aircraft interior noise

    Crane, Scott / Cunefare, Kenneth / Engelstad, Stephen et al. | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

      A comparison of optimization formulations for design minimization of aircraft interior noise

      Crane, S.P. / Cunefare, K.A. / Engelstad, S.P. et al. | Tema Archive | 1996
      were subject to upper and lower bounds on the design variables, the structural shell element thickness. All analyses were performed at a single ...
      Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston

    A Comparison of Probabilistic and Lower Bound Methods for Predicting the Response of Buckling Sensitive Structures

    Arbocz, J. / Nemeth, M. P. / Starnes, J. H. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    A Comparison of Three Algorithms for Tracing Nonlinear Equilibrium Paths of Structural Systems

    Gurdal, Z. / Ragon, S. A. / Watson, L. T. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    A Complex Velocity Solution fo the Flutter Equations

    Pitt, D. M. / American Institute of Aeronautics and Astronautics / American Society of Mechanical Engineers et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    A Composite Support Structure for a Membrane Mirror

    Black, Jonathan / deBlonk, Brett / Patrick, Brian et al. | AIAA | 2005
    Publisher: The American Institute of Aeronautics and Astronautics

    A Composite Wing Structure with a Morphing Leading Edge

    Morishima, Ryoko / Guo, Shijun / Ahmed, Shakeel | AIAA | 2010
    Publisher: The American Institute of Aeronautics and Astronautics

      A Composite Wing Structure with a Morphing Leading Edge

      Morishima, R. / Guo, S. / Ahmed, S. et al. | British Library Conference Proceedings | 2010
      Publisher: American Institute of Aeronautics and Astronautics , Reston, Va.
      Keywords: Structural dynamics , Materials

    A Conceptual Aerospace Vehicle Structural System Modeling, Analysis and Design Process

    Mukhopadhyay, Vivek | NTRS | 2007
    scenarios are generated for analyzing several structural configurations and material alternatives. The structural stress, deflection, strain, and ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    A coupled fluid-structure dynamic analysis for water impact loads

    HERTING, D. | AIAA | 1975
    Publisher: The American Institute of Aeronautics and Astronautics

    Acoustic Control of a Rocket Fairing Using Spatially Weighted Transducer Arrays

    Clark, R. L. / Griffin, S. F. / Kemp, J. D. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Acoustic vibration model for a composite shell with sound absorption material

    Dungan, Michael / Anderson, William / Mollo, Christopher et al. | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

    Acoustic vibration model of a composite shell with sound absorption material

    Dungan, M.R. / Mollo, C. / Vlahopoulos, N. et al. | Tema Archive | 1996
    only in two dimensions. This formulation assumes an isotropic structural member that couples with the elastic porous material. To expand beyond ...
    Publisher: American Institute of Aeronautics and Astronautics (AIAA) , Reston
    Keywords: poröser Werkstoff , Scherung (Werkstoff)

    A criterion to judge the accuracy of frequency domain approximating functions

    SCHWANZ, R. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    ACSR system for vibration suppression in coupled helicopter rotor/flexible fuselage model

    Chiu, Thiem / Friedmann, Peretz | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

    Active Aeroelastic Tailoring of High Aspect Ratio Composite Wings

    Cesnik, C. E. S. / Ortega Morales, M. / Patil, M. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Active Aeroelastic Tailoring with Adaptive Continuous Control Surfaces

    Dobbins, A. / Duke, D. K. / Weisshaar, T. A. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Active Control for Elastic Wing Structure Dynamic Modes

    Urnes, James M. / Dykman, John R. / Truong, Hieu | AIAA | 2015
    Publisher: The American Institute of Aeronautics and Astronautics

    Active Control for Elastic Wing Structure Dynamic Modes (AIAA 2015-1842)

    Urnes, James M. / Dykman, John R. / Truong, Hieu | British Library Conference Proceedings | 2015

    Active Control of Airframe Response with Distributed Smart Actuators

    Chopra, I. / Park, H. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Active control of a structure with two closely spaced natural frequencies

    XU, K. / WARNITCHAI, P. / IGUSA, T. | AIAA | 1992
    Publisher: The American Institute of Aeronautics and Astronautics

    Active Control of Inflatable Structure Membrane Wrinkles Using Genetic Algorithm and Neural Network

    Peng, Fujun / Hu, Yan-Ru / Ng, Alfred | AIAA | 2004
    Publisher: The American Institute of Aeronautics and Astronautics

    Active Control of Vibration in Carbon Re-Enforced Composites Using Embedded Piezo-Ceramics

    Giovanardi, M. / Herrick, J. / Pletner, B. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Active damping of a large lightweight structure using piezoelectric sensors and actuators

    FREYMANN, RAYMOND / STUEMPER, EDMOND | AIAA | 1991
    Publisher: The American Institute of Aeronautics and Astronautics

    Active damping of modal vibrations by force apportioning

    HALLAUER, JR., W. / BARTHELEMY, J.-F. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Active Flow Control Using Microelectromechanical Systems

    Chen, P. / DeVoe, D. / Kiddy, J. et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Active flutter suppression control law definition via least squares synthesis

    JOHNSON, E. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Active flutter suppression on an F-4F aircraft

    SENSBURG, O. / HOENLINGER, H. / NOLL, T. et al. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Active flutter suppression using MIMO adaptive LMS control

    Eversman, Walter / Danda Roy, Indranil | AIAA | 1996
    Publisher: The American Institute of Aeronautics and Astronautics

    Active-member control of precision structures

    Fanson, J. L. / Blackwood, G. H. / Chu, C. C. | NTRS | 1989
    precision truss structure. These experiments are directed toward the development of high performance structural systems as part of the Control ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Spacecraft Design, Testing And Performance

    Active member vibration control for a 4 meter primary reflector support structure

    UMLAND, J. / CHEN, G.-S. | AIAA | 1992
    Publisher: The American Institute of Aeronautics and Astronautics

    Active robust shape control of flexible structure

    Hu, Yan-Ru / Vukovich, G. | Tema Archive | 2003
    , and space station, etc. The flexibility of these large space structures results in problems of structure shape deformation and vibration, etc ...

    Active Robust Vibration Control of a Circular Plate Structure Using Piezoelectric Actuators

    Hu, Yan-Ru / Ng, Alfred | AIAA | 2002
    Publisher: The American Institute of Aeronautics and Astronautics

      Active Robust Vibration Control of a Circular Plate Structure Using Piezoelectric Actuators

      Hu, Y. / Ng, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002
      Keywords: structural dynamics , materials

    Active Structural Acoustic Control of Noise Transmission into a Cylindrical Enclosure

    Clark, R. / Henry, J. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 2000
    Keywords: structural dynamics

    Active vibration control in rotorcraft systems using smart actuators

    Anderson, G.L. / Garg, D.P. | Tema Archive | 2002
    the structure. A smart structure is generally composed of a number of distributed sensors and actuators embedded and/or surface-mounted on a ...