1–20 of 120 hits
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    Synthesis of structural damping.

    Bieber, R. E. / Chang, C. S. | NTRS | 1968
    Force deflection relationship under arbitrary loading for structure exhibiting hysteresis behavior ...
    Keywords: Structural Mechanics

    Honeycomb sandwich joints for primary structure

    SOUDAK, U. / HAMM, R. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Built-up low-cost advanced titanium structures /BLATS/

    FRANKLIN, W. / WAITZ, C. | AIAA | 1980
    Publisher: The American Institute of Aeronautics and Astronautics

    Revision of maximum stress criterion of combined modes of fracture

    WANG, T. / TU, S.-Y. | AIAA | 1980
    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

    Crash energy absorbing composite sub-floor structure

    FARLEY, G. | AIAA | 1986
    Publisher: The American Institute of Aeronautics and Astronautics

    Designing Space Station structure for assembly

    RIEL, F. | AIAA | 1988
    Publisher: The American Institute of Aeronautics and Astronautics

    Durability prediction of complex panels with fluid-structure interaction

    FERMAN, M. / HEALEY, M. / RICHARDSON, M. | AIAA | 1988
    Publisher: The American Institute of Aeronautics and Astronautics

    The analysis of a composite shell structure

    PALAZOTTO, A. / OLSEN, J. | AIAA | 1989
    Publisher: The American Institute of Aeronautics and Astronautics

    Locating damaged members in a truss structure using modal test data - A demonstration experiment

    SMITH, SUZANNE / MCGOWAN, PAUL | AIAA | 1989
    Publisher: The American Institute of Aeronautics and Astronautics

    Probabilistic analysis of a materially nonlinear structure

    MILLWATER, H. / WU, Y.-T. / FOSSUM, A. | AIAA | 1990
    Publisher: The American Institute of Aeronautics and Astronautics

    ADAPTIVE ADJUSTMENT OF A PRECISION TRUSS STRUCTURE: EXPERIMENTAL VALIDATION

    SALAMA, M. / UMLAND, J. / BRUNO, R. et al. | AIAA | 1993
    Publisher: The American Institute of Aeronautics and Astronautics

    ESTIMATING FREE-BODY MODAL PARAMETERS FROM TESTS OF A CONSTRAINED STRUCTURE

    COOLEY, VICTOR | AIAA | 1993
    Publisher: The American Institute of Aeronautics and Astronautics

    Effects of geometric nonlinearities on the response of optimized box beam structures

    Ragon, S. / Gurdal, Z. | NTRS | 1993
    analysis. In all cases, the structure collapses below the design load, and does so in a mode which differs from that of linear theory. This ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Structural Mechanics

    Nonclassical aileron buzz in transonic flow

    Bendiksen, Oddvar O. | NTRS | 1993
    formulation is used to model the fluid-structure system and to obtain a system of space-discretized equations that is time-marched to simulate the ...
    Publisher: NASA National Aeronautics and Space Administration
    Keywords: Structural Mechanics

    System identification of the JPL micro-precision interferometer truss - Test-analysis reconciliation

    Red-Horse, J. R. / Marek, E. L. / Levine-West, M. | NTRS | 1993
    -verified analytical structural models. This paper focuses on one aspect of the effort to produce such a model for the MPI structure, test-analysis ...
    Publisher: American Institute of Aeronautics and Astronautics
    Keywords: Structural Mechanics

    Damage tolerance of composite sandwich structure

    Baron, William / Smith, W / Czarnecki, Gregory | AIAA | 1995
    Publisher: The American Institute of Aeronautics and Astronautics

    An experimental study for damage detection using a hexagonal truss structure

    Kim, Hyoung / Bartkowicz, Theodore | AIAA | 1995
    Publisher: The American Institute of Aeronautics and Astronautics

    Low cost composite fabrication methods applied to low observable structure

    Guy, Teresa / Sanger, Kenneth / Ruskowski, Ed | AIAA | 1995
    Publisher: The American Institute of Aeronautics and Astronautics

    The influence of friction models on passive damping and dynamic response of a flexible beam structure

    Bindemann, Alan / Ferri, Aldo | AIAA | 1995
    Publisher: The American Institute of Aeronautics and Astronautics