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A Dynamic Response Analysis Method Based on Dual Mode Equation in Random Noise Environment

A random noise and analysis method technology, which is applied in special data processing applications, measurement of ultrasonic/sonic/infrasonic waves, complex mathematical operations, etc., can solve problems such as errors and waste of computing resources, so as to save design costs, shorten design cycles, and improve The Effect of Dynamic Response Predicting Efficiency

Active Publication Date: 2018-08-21
SOUTHEAST UNIV
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Problems solved by technology

[0003] When predicting the dynamic response of the system under random noise excitation based on the dual mode equation theory, it is necessary to intercept the subsystem modes within a limited frequency range to participate in the response prediction. Too few selected modes will cause errors, and too many modes will be selected. Will cause waste of computing resources

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  • A Dynamic Response Analysis Method Based on Dual Mode Equation in Random Noise Environment
  • A Dynamic Response Analysis Method Based on Dual Mode Equation in Random Noise Environment
  • A Dynamic Response Analysis Method Based on Dual Mode Equation in Random Noise Environment

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[0048] The present invention will be further described below in conjunction with the accompanying drawings.

[0049] figure 1 It is a logic flow diagram of the present invention, comprising steps:

[0050] Step (1) Divide the structure and acoustic cavity in the acoustic-solid coupling system into different subsystems; the acoustic-solid coupling system is a coupling system between the structure and the acoustic cavity, and there is an interaction between the structural vibration and the sound pressure fluctuation of the sound field; The boundary conditions on the interface are approximated, the boundary conditions of the structural subsystem on the coupling interface are approximated as free states, and the boundary conditions of the acoustic cavity subsystem on the coupling interface are approximated as fixed boundaries.

[0051]Step (2) Calculate the modes of the structural subsystem and the acoustic cavity subsystem whose natural frequency is lower than 1.25 times the upp...

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Abstract

A dynamic response analysis method based on a dual-mode equation in a random noise environment includes the following steps: (1) dividing a structure and an acoustic cavity in an acoustic-structural coupling system into different subsystems; (2) calculating modes of the structural subsystems and the acoustic cavity subsystems; (3) calculating inter-mode coupling parameters in adjacent subsystems; (4) establishing a dual-mode equation of the coupling system; (5) by means of pre-processing, obtaining a cross power spectrum of generalized force loads applied on the subsystem modes under the action of a random load; (6) calculating the dual-mode equation to obtain cross power spectra of all participation factors of all modes; and (7) by means of modal superposition, calculating a random acoustic-structural coupling response of the system.

Description

technical field [0001] The invention relates to the technical field of acoustic-solid coupling response prediction, in particular to a dynamic response analysis method based on a dual mode equation in a random noise environment. Background technique [0002] As the spacecraft develops to a high flight speed, it faces severe random noise and other environments during the mission cycle, which may cause structural failure or failure of precision instruments and instruments. Therefore, in the design process of the spacecraft, the influence of random noise needs to be considered. Experimental method, theoretical method and numerical method can be used to predict the dynamic response of the system under random noise excitation. Among them, the test method can obtain reliable results, but the cost of carrying out test analysis is high and the design cycle is long; the theoretical method is only suitable for simple systems, and it is difficult to solve the problem of dynamic respon...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50
CPCG06F30/15G06F30/20G01H17/00G06F17/13Y02T90/00G06F17/16G06F30/23
Inventor 李彦斌张鹏费庆国吴邵庆杨轩姜东
Owner SOUTHEAST UNIV
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