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  • STRUCTURAL MECHANICS  (3)
  • FLUID MECHANICS AND HEAT TRANSFER
  • barley
  • 1985-1989  (3)
  • 1
    Publication Date: 2019-06-28
    Description: The effects of nonlinear damping on the large-deflection response of symmetrically laminated composite panels is studied by time-domain simulation in an attempt to quantify experimentally observed phenomena. A single-mode deflection approach is used in the equations of motion and in the linear and nonlinear damping models. The probability, peak-probability, and spectral-density data are compiled for both strains and deflection. The rms responses as a function of input excitation level are also obtained and compared to linear, equivalent-linearization, and Fokker-Planck equation solutions.
    Keywords: STRUCTURAL MECHANICS
    Type: AIAA PAPER 89-1104
    Format: text
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  • 2
    Publication Date: 2019-07-13
    Description: Results of a preliminary investigation into a method which can be used to improve the results of an experimental force prediction analysis is presented. The method uses a singular value decomposition technique to reduce measurement noise present in the measured input data matrix. The fundamental theory for the method along with an experimental example is shown. The method is shown to provide encouraging force prediction improvements when the input data matrix contains high levels of measurement noise.
    Keywords: STRUCTURAL MECHANICS
    Type: International Modal Analysis Conference; Feb 01, 1988 - Feb 04, 1988; Kissimmee, FL; United States
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  • 3
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    In:  Other Sources
    Publication Date: 2019-07-13
    Description: The purpose of this paper is to present the results of a preliminary investigation of an indirect method which can be used to generate a set of equivalent point loads approximating an applied distributed acoustic load. The method combines the source information with the structure's modal characteristics and forces which give the same response as the applied acoustic load. The technique is demonstrated by predicting a set of point forces acting on a thin aluminum panel which simulate a normally-incident random pressure. The technique is verified by comparing measured strain autospectrums with estimated strain autospectrums generated using the predicting forces. Strain errors within 5 dB were achieved. A limited amount of information about the acoustic load could be deduced using the predicted force autospectrums and phase differences between these forces.
    Keywords: STRUCTURAL MECHANICS
    Type: International Modal Analysis Conference; Feb 01, 1988 - Feb 04, 1988; Kissimmee, FL; United States
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