5篇
您的检索式：作者名="Fangsen CUI"
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| 1 | Nonlinear Finite Element Simulations to Elucidate the Determinants of Perforator Patency in Propeller Flaps显示文摘 | Chin-Ho Wong Fangsen Cui Bien-Keem Tan Zhuangjian Liu Heow-Pueh Lee C Lu Chee-Liam Foo Colin Song | 2007 | Annals of Plastic Surgery2007，，6： | 2 |
| 2 | Bifurcation and Chaos in the Du f f ing Oscillator with a PID 显示文摘 | Fangsen Cui Chew C H Jian X X | 1997 | Controller Nonlinear Dynamics1997，12，： | 1 |
| 3 | Bifurcation and chaos in the duffing oscillator with a pid controller显示文摘 | Cui Fangsen Chew C H | 1997 | Nonlinear Dynamics1997，12，3： | 1 |
| 4 | Bifurcation and Chaos in the Duffing Oscillator with a PID Controller显示文摘 | Cui Fangsen CH Chew Xu Jian xue | 1997 | International Journal of Non-Linear Mechanics1997，，24： | 1 |
| 5 | Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network显示文摘Manmade debris and natural meteoroids, travelling in the Low Earth Orbit at a speed of several kilometers per second, pose a severe safety concern to the spacecraft in service through the HyperVelocity Impact(HVI). To address this issue, an investigation of shock Acoustic Emission(AE) waves induced by HVI to a downscaled two-layer Whipple shielding structure is performed,to realize a quantitative damage evaluation. Firstly a hybrid numerical model integrating smoothparticle hydrodynamics and finite element is built to obtain the wave response. The projectiles, with various impact velocities and directions, are modelled to impact the shielding structure with different thicknesses. Then experimental validation is carried out with built-in miniaturized piezoelectric sensors to in situ sense the HVI-induced AE waves. A quantitative agreement is obtained between numerical and experimental results, demonstrating the correctness of the hybrid model and facilitating the explanation of obtained AE signals in experiment. Based on the understanding of HVI-induced wave components, assessment of the damage severity, i.e., whether the outer shielding layer is perforated or not, is performed using the energy ratio between the regions of ‘‘high frequency' and ‘‘low frequency' in the acquired AE signals. Lastly, the direct-arrival fundamentalsymmetric wave mode is isolated from each sensing signal to be input into an enhanced delay-andsum algorithm, which visualizes HVI spots accurately and instantaneously with different sensor network configuration. All these works demonstrate the potential of quantitative, in situ, and real time HVI monitoring using miniaturized piezoelectric sensor network. | Menglong LIU Qiang WANG Qingming ZHANG Renrong LONG Fangsen CUI Zhongqing SU | 2019 | Chinese Journal of Aeronautics2019，32，5： | 1 |
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