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地球等离子体片中爆震流的理论研究
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作者 陈出新 《地球科学进展》 CAS CSCD 2001年第4期584-586,共3页
地球等离子体片中持续时间很短的快速流动事件最近受到很多关注。这些事件被An gelopoulos等称为爆震流 ,简要回顾了爆震流的理论研究。当前理论认为 ,爆震流是磁泡 (含较少等离子体的磁流通管 )在交换不稳定性的作用下在等离子体片中... 地球等离子体片中持续时间很短的快速流动事件最近受到很多关注。这些事件被An gelopoulos等称为爆震流 ,简要回顾了爆震流的理论研究。当前理论认为 ,爆震流是磁泡 (含较少等离子体的磁流通管 )在交换不稳定性的作用下在等离子体片中的流动。磁泡图像很自然地解释了等离子体片中观测到的爆震流。理论预期的快速流在横穿磁尾方向的尺度 ,它的速度伴随着磁场松弛。 展开更多
关键词 等离子体片 爆震流 磁泡 磁流通管 电离层 等离子体压力
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A Blast Shock Isolation System with MRFD and Its Semi-Active Control Analysis
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作者 LIU Jingbo WANG Libin DU Yixin WANG Yan 《Transactions of Tianjin University》 EI CAS 2006年第B09期65-69,共5页
To effectively reduce the damage to people and devices in civil defense engineering subjected to blast shock, a blast shock isolation system with magnetorheological fluid dampers (MRFD) is proposed. MRFD can provide c... To effectively reduce the damage to people and devices in civil defense engineering subjected to blast shock, a blast shock isolation system with magnetorheological fluid dampers (MRFD) is proposed. MRFD can provide continuously adjustable Coulomb friction and has many advantages for semi-active control. Numerical simulation of this isolation system is finished using Matlab simulink toolbox. General semi-active control algorithms are consided based on instantaneous optimal active control algorithm. And the results indicate that the shock isolation system can work efficiently, decreasing about 93% of the peak acceleration of the isolation floor. 展开更多
关键词 blast shock ISOLATION magnetorheological fluid damper semi-active control SIMULINK
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Numerical Investigation on Detonation Wave through U-bend 被引量:3
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作者 Shinobu Otsuka Masaya Suzuki Makoto Yamamoto 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第6期540-544,共5页
Pulse detonation engine (PDE) is expected for a next-generation propulsion system. PDE is a promising engine that can generates power and thrust by using intermittent detonation. Promotion of deflagration to detonatio... Pulse detonation engine (PDE) is expected for a next-generation propulsion system. PDE is a promising engine that can generates power and thrust by using intermittent detonation. Promotion of deflagration to detonation transition (below DDT) is a key issue to realize this system. PDE has experimentally been investigated, and it was confirmed that detonation tubes with U-shaped bends are useful for fast DDT. However, the mechanism of DDT promotion due to U-bends has not been well clarified. In the present study, the influence of a U-bend on detona-tion wave propagation is researched with computational fluid dynamics (CFD). The numerical results show that detonation wave disappears once near the U-bend inlet and restarts after passing through it. In addition, it was found that the use of the U-bend with small channel width and curvature radius can induce fast DDT. 展开更多
关键词 DETONATION Deflagration to Detonation Transition (DDT) U-bend Computational Fluid Dynamics
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