Optimal design method for reducing transient acoustic radiation of plate structure
A technology for optimizing design and sound radiation, applied in the direction of design optimization/simulation, calculation, instrument, etc., can solve unlikely problems, and achieve the effect of reducing transient sound radiation and realizing transient radiation sound pressure
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Embodiment 1
[0040] Embodiment one (structural schematic diagram sees figure 2 and image 3 ) The specific optimization steps are as follows:
[0041] Step 1. Based on the time-domain finite element-boundary element coupling method, establish a theoretical calculation equation for the transient sound radiation of a flat plate structure suitable for any boundary conditions:
[0042]
[0043] The derivation of the above formula is based on the time-domain finite element-boundary element coupling method, where SPL max is the maximum instantaneous radiated sound pressure level of the flat plate structure, p(ξ,t) is the instantaneous radiated sound pressure at ξ position at time t; S p is the plate area, ρ 0 is the air density, x is the coordinates of the plate nodes, c is the speed of sound, {R} is the transformation matrix, which is used to convert the node displacement of the plate structure into the transverse deflection, δ is the Dirac function, is the instantaneous nodal accelera...
Embodiment 2
[0087] Step 1. Based on the time-domain finite element-boundary element coupling method, establish a theoretical calculation equation for the transient sound radiation of a flat plate structure applicable to any boundary conditions;
[0088] Step 2. Set various known parameters of the plate structure, including plate material, plate damping factor, plate size and plate thickness, and set the specific position ξ for calculating the instantaneous radiated sound pressure. In this embodiment, ξ is set at a position 1m away from the flat structure on the center normal of the flat structure; the specific parameter values of the set flat structure are shown in the following table:
[0089]
[0090]
[0091] Step 3. Set the adjustable range of boundary parameters, as shown in the table below:
[0092]
[0093] Step 4. The initial state of the plate structure and the transient excitation received are given. The initial state given in this example is The center of the plat...
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Abstract
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Application Information
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