Authors: Xiao Tong Chang, Yun Ju Yan
Abstract: Missiles always undergo non-stationary and continuously distributed load. However, only some centralized loads can be adopted in the ground for their vibration experiments. In this paper, the theoretical analysis and numerical simulation computations programs are established for the distributed and non-stationary airdynamic load being translated into several equivalent centralized loads for high-speed missile. The researches showed that, under the equivalent rule of structural modal responses, the average responses error in both domains time and frequency is within 1.5dB, so it is possible to provide a feasible method for the vibration test on the ground for missile structures.
965
Authors: Long Yu, Yun Ju Yan, Jie Sheng Jiang, Li Cheng
Abstract: A method based on entropy-based criteria is present to choose the optimal decomposition
of Wavelet Packets Analysis (WPA) for damage detection in composite materials. The structural
damage indexes constructed based on energy spectrum variation of the structural vibration responses
decomposed using WPA before and after the occurrence of structural damage usually generate a
complete binary tree to calculate its elements. Date mining is carried out in this paper by adoption
entropy as the criteria to choose the optimal decomposition tree. In the decomposition process, only
the sub-signals which contain main information of the original signal are decomposed to generate
next level sub-signals. New damage index is constructed based on the optimal decomposition. Then
the dimension of the damage index is reduced while still keeping its sensitive to damage. Whether
Artificial Neural Network (ANN) or genetic algorithm (GA) is used in the further process of telling
structural damage status from damage index, this reduction will make remarkable time saving.
1149
Authors: Yun Ju Yan, Huan Guo Chen, Jie Sheng Jiang
Abstract: Sensor data are the basis for health assessment of complex structural systems. Careful
selection and logical layout of sensors is critical to enable the high reliability of system health
assessment. This paper presents a methodology how to use a minimum number of sensors, and what
locations of them should be placed, so that the voltage signals received from the sensor can be used to
detect both presence and extent of damage. In this study, an optimization procedure is developed
using Genetic Algorithm (GA) to determine the location of piezoelectric sensor for damage detection
in a composite wingbox. A new damage index using all differences in voltage signals decomposed by
wavelet transform is proposed. Results show that the proposed method is available at determining
number and location of sensors for structural damage detection using piezoelectric patch sensors.
1033
Authors: Xu Ge, Yun Ju Yan, Huan Guo Chen
Abstract: The paper presents an effective damage detection method of complex composite structures.
It can be carried out through the experimental modal analysis of the damaged structure. The method
using the improved Cross Modal Strain Energy (CMSE) technique and Niche GA has many
advantages compared with other damage detection methods. The CMSE method can use any modes
of the structure and the modes don’t need to be normalized or consistent in scale. The Niche GA
improves the efficiency of the calculation and enhances the capacity of identifying structural damage
localization. The model is the composite material airfoil case. The numerical results show that the
method proposed in this paper is successful for damage detection of complex structures.
929
Authors: Huan Guo Chen, Yun Ju Yan, Jie Sheng Jiang
Abstract: A vibration-based approach to detect crack damage in a cantilever composite wingbox is
studied using the improved Hilbert-Huang Transform (HHT). The improved HHT is composed of
HHT with Wavelet Packet Transform (WPT) and a simple but effective method for intrinsic mode
function (IMF) selection. For different damage status, in order to obtain structural dynamic responses,
which imply plentiful damage information, the composite wing boxes were excited by a contrived
square wave signal. Then, the dynamic responses of intact wingbox and damaged wingbox are
disposed using improved HHT. Finally, a feature index vector of structural damage, i.e. the ariation
quantity of instantaneous energy, is constructed. The obtained results show that the proposed damage
feature index vector is more sensitive to small damage than those in traditional signal processing.
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