Abstract:It is often desirable to simultaneously optimize the damping and stiffness distribution in the design of shell structures incorporating damping material layers for achieving the best vibration mitigation performance. This paper investigates the integrated topology optimization of host structures and damping layers for reducing the vibration level in the presence of harmonic excitations. Therein, the global damping matrix is a nonproportional one due to distributed damping effects. For an efficient frequency re… Show more
“…Kang et al [18] proposed an optimization methodology based on frequency response analysis. They also extended their work to simultaneous optimization of the damping and host layers [19]. An experimental verification of these works has also been reported [20].…”
Section: Introductionmentioning
confidence: 85%
“…In addition to the maximizing the imaginary part of the dynamic compliance (abbreviated as IDC hereafter) in Eq. (13), we also minimize the amplitude of the loading point (abbreviated as AMP hereafter), which is a typical objective function in damping material optimization based on frequency response [18,19].…”
Section: D Cantilever Examplementioning
confidence: 99%
“…Of these approaches, we focus on frequency response-based optimization, which is more straightforward than the eigenfrequency-based method when the excitation frequency can be predicted. A typical objective function proposed in previous research is minimization of the amplitude of the loading domain [18,19,21]. However, in actual mechanical design, the damping material is usually used to reduce the response peak at resonance near the excitation frequency rather than the response under the specified single frequency.…”
In this research, we propose a new objective function for optimizing damping materials to reduce the resonance peak response in the frequency response problem, which cannot be achieved using existing criteria. The dynamic compliance in the frequency response problem is formulated as the scalar product of the conjugate transpose of the amplitude vector and the force vector of the loading nodes. The proposed objective function methodology is implemented using the common solid isotropic material with penalization (SIMP)
“…Kang et al [18] proposed an optimization methodology based on frequency response analysis. They also extended their work to simultaneous optimization of the damping and host layers [19]. An experimental verification of these works has also been reported [20].…”
Section: Introductionmentioning
confidence: 85%
“…In addition to the maximizing the imaginary part of the dynamic compliance (abbreviated as IDC hereafter) in Eq. (13), we also minimize the amplitude of the loading point (abbreviated as AMP hereafter), which is a typical objective function in damping material optimization based on frequency response [18,19].…”
Section: D Cantilever Examplementioning
confidence: 99%
“…Of these approaches, we focus on frequency response-based optimization, which is more straightforward than the eigenfrequency-based method when the excitation frequency can be predicted. A typical objective function proposed in previous research is minimization of the amplitude of the loading domain [18,19,21]. However, in actual mechanical design, the damping material is usually used to reduce the response peak at resonance near the excitation frequency rather than the response under the specified single frequency.…”
In this research, we propose a new objective function for optimizing damping materials to reduce the resonance peak response in the frequency response problem, which cannot be achieved using existing criteria. The dynamic compliance in the frequency response problem is formulated as the scalar product of the conjugate transpose of the amplitude vector and the force vector of the loading nodes. The proposed objective function methodology is implemented using the common solid isotropic material with penalization (SIMP)
“…e optimization objective function is to minimize the structural vibration at specified positions, and the steady-state response of the vibrating structure is obtained by using the complex mode superposition method in the state space to deal with the nonproportional damping. Zhang and Kang [11] proposed an optimization methodology based on the frequency response analysis, and they extended their work to simultaneous optimization of the damping and host layers. Fang and Zheng [12] proposed a topology optimization method to minimize the resonant response of plates with CLD treatment at specified broadband harmonic excitations and studied the effect of the modal sensitivity analysis on optimization of the damping material.…”
This paper deals with an optimal layout design of the constrained layer damping (CLD) treatment of vibrating structures subjected to stationary random excitation. The root mean square (RMS) of random response is defined as the objective function as it can be used to represent the vibration level in practice. To circumvent the computationally expensive sensitivity analysis, an efficient optimization procedure integrating the pseudoexcitation method (PEM) and the double complex modal superposition method is introduced into the dynamic topology optimization. The optimal layout of CLD treatment is obtained by using the method of moving asymptote (MMA). Numerical examples are given to demonstrate the validity of the proposed optimization procedure. The results show that the optimized CLD layouts can effectively reduce the vibration response of the structures subjected to stationary random excitation.
“…However, the study was only focused on flat panel and shell, not on stiffened panels. Based on this, Zhang et al 20 proposed the integrated topology optimization of host structures and damping layers to reduce vibration levels in the presence of harmonic excitations. During the optimization process, the localized modes in low-density areas were avoided.…”
This paper studies topology optimization of metallic and composite panels of three different configurations (flat,
three-bay and 3×3 grid) covered by the constrained damping materials considering first modal loss factors. The
vibration experiments seek to obtain the first modal loss factor and first modal frequency for the aforementioned
panels, and corresponding finite element (FE) simulations are completed using commercial software ABAQUS
R
.
According to simulation results, the distribution of constrained damping materials is optimized with evolutionary
structural optimization (ESO) method developed using MATLAB. The results show that the first modal loss
factors of optimized panels are reduced slightly if the constrained damping material is removed by 50%. Under
the base excitation near each first modal frequency, the maximum root mean square of Von Mises equivalent
stress (RMISES) of optimized flat panels and 3×3 grid stiffened panels decreases compared with panels without
constrained damping materials. However, the maximum RMISES value of optimized three-bay stiffened panels
nearly remains unchanged due to the configuration type of the stiffeners. These results conclude that the three-bay
stiffened panel is the best to reduce the maximum RMISES value of at base structure with the same additional
mass
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