Influences of the temperature rise on the vibration energy flow in a dissipative elastic metamaterial plate based on the structural intensity approach

2021 ◽  
Vol 160 ◽  
pp. 107347
Author(s):  
Tao Chen ◽  
Liangmei Liu ◽  
Qiunan Liu ◽  
Fuxin Song ◽  
Zhiwei Feng
2015 ◽  
Vol 12 (03) ◽  
pp. 1550013 ◽  
Author(s):  
Siu-Siu Guo ◽  
Dongfang Wang ◽  
Zishun Liu

The concept of structural intensity (SI) is extended to the random domain by introducing a physical quantity denominated random structural intensity (RSI). This quantity is formulated for mechanical systems whose dynamical responses are stochastic due to random excitations. In order to fully characterize the stochastic behavior of a system under random loadings, it is imperative to obtain the probability density function (PDF) of RSI. Based on the elastic theory and the definition of SI, RSI is expressed as functions of system responses. In general, the PDF of system responses is governed by Fokker–Planck–Kolmogorov (FPK) equation under the assumption that random dynamic loadings are idealized as white noise excitations. Therefore, the PDF of RSI is derived with the joint PDF of system responses. In the present study, four demonstrating cases of beams and plates under separately concentrated and uniform random loadings are studied to investigate the properties of RSI. Stationary and non-stationary PDFs of RSI at arbitrary section of beam and plate are obtained. Numerical results show that the PDF of RSI is transient at early stage of stationary loading and then converges to the exact stationary ones as time increases. With the obtained PDFs of RSI, energy transmission path over the beam and plate can be determined, which is guided from the locations with lower probabilities of RSI to the ones with higher probabilities of RSI. Furthermore, virtual energy flow sinks on the plate and beam can be found, which are identified by the locations with the maximum probabilities of RSI.


2012 ◽  
Vol 78 (789) ◽  
pp. 988-992
Author(s):  
Toru YAMAZAKI ◽  
Takamasa SONE ◽  
Takashi HASHIMOTO ◽  
Katsuhiko KURODA
Keyword(s):  

2011 ◽  
Vol 2011.21 (0) ◽  
pp. 86-89
Author(s):  
Toru YAMAZAKI ◽  
Takamasa SONE ◽  
Takashi HASHIMOTO ◽  
Katsuhiko KURODA
Keyword(s):  

2002 ◽  
Vol 2002 (0) ◽  
pp. 43-44
Author(s):  
Kouki Shiohata ◽  
Kazutaka Tanaka ◽  
Toru Yamazaki

2013 ◽  
Vol 2013.19 (0) ◽  
pp. 149-150
Author(s):  
Atsushi KITAHARA ◽  
Takuya YOSHIMURA ◽  
Yusuke NAKAMURA

1998 ◽  
Vol 217 (1) ◽  
pp. 43-74 ◽  
Author(s):  
C.S. Manohar ◽  
S. Adhikari
Keyword(s):  

2019 ◽  
Vol 39 (2) ◽  
pp. 313-326
Author(s):  
Yingqun Ma ◽  
Qingjun Zhao ◽  
Kai Zhang ◽  
Meng Xu ◽  
Wei Zhao

The main goal of the study is to apply the structural intensity method to analyze the effects of positions of the main-mount and the sub-mount on the vibrational energy flow transmission characteristics in aero-engine casing structures, so as to attenuate the vibration of the casing and the whole aero-engine. Structural intensity method, indicating magnitude and direction of the vibrational energy flow, is a powerful tool to study vibration problems from the perspective of energy. In this paper, a casing-support-rotor coupling model subjected to the rotor unbalanced forces is established by the finite element method. Formulations of the structural intensity of a shell element and the structural intensity streamline are given. A simulation system consisting of the finite element tool and the in-house program is developed to carry out forced vibration analysis and structural intensity calculation. The structural intensity field of the casing is visualized in the forms of vector diagram and streamline representation. The vibrational energy flow behaviors of the casing at the rotor design rotating speed are analyzed, and the vibrational energy flow transmission characteristics of the casing with different axial positions of the main-mount and the sub-mount are investigated. Moreover, some measures to attenuate the vibration of the casing are obtained from the numerical results, and their effectiveness is verified in the frequency domain and the time domain. The results shed new light on the effects of the mount positions on the vibration energy transmission behaviors of the casing structure. The structural intensity method is a more advanced tool for solving vibration problems in engineering. Furthermore, it may provide some guidance for the vibration attenuation of the casing and the whole aero-engine.


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