Hyperloop has become one of the key reserve technologies for future high-speed rail transit.The gas in the tube is compressed and rubbed,leading to a strong aerodynamic heating effect.The research on the flow field ch...Hyperloop has become one of the key reserve technologies for future high-speed rail transit.The gas in the tube is compressed and rubbed,leading to a strong aerodynamic heating effect.The research on the flow field characteristics and aerodynamic heating effect of hyperloop is in its infancy,and that on the flow field structure is lacking.In this study,the nozzle theory was used to make a preliminary judgment on the choked flow phenomenon in the hyperloop.Based on the flow results obtained under different working conditions,the identification basis of the choked flow phenomenon in the hyperloop was obtained.Furthermore,the effect of the choked/unchoked flow on the flow structure,temperature,and pressure distribution of the annular space in the tube was analyzed.Based on traditional high-speed railway aerodynamics,according to relevant theories and calculation in aerospace field,and combined with the model test data,the reliability verification analysis on the characteristics of the flow field are carried out.The structure of the flow filed in the tube can be divided into choked and unchoked.The judgment is dependent on whether the throat reaches the speed of sound.Under the choked flow,a normal shock wave is formed in front of the tube train.The temperature rise of the local flow field exceeds 50 K;the temperature rise of the stagnation region exceeds 88 K,and the pressure is approximately 1.7 times that of the initial pressure in the tube.When the flow is unchoked,differences arise in the distribution of the flow field corresponding to different incoming Mach numbers.When the incoming flow is supersonic,the flow field maintains a supersonic speed,and a bow-shaped shock wave is formed at the front of the tube train.Owing to the shock wave or expansion wave,the local flow field exhibits significant fluctuations in temperature and pressure.Conversely,when the incoming flow is subsonic,the flow field in the tube maintains a subsonic speed,and no shock wave structure is observed.展开更多
Bit Torrent文件共享系统中的搭便车(free-riding)节点会使系统性能大幅下降,目前,Bit Torrent主要采用choking策略来抑制搭便车行为,但与choking合作而存在的随机选择节点的unchoking策略仍然给搭便车行为提供了机会.提出了一种基于概...Bit Torrent文件共享系统中的搭便车(free-riding)节点会使系统性能大幅下降,目前,Bit Torrent主要采用choking策略来抑制搭便车行为,但与choking合作而存在的随机选择节点的unchoking策略仍然给搭便车行为提供了机会.提出了一种基于概率连接交换(probabilistic link exchange,简称PLX)的unchoking策略,在实现unchoking功能的同时,有效地抑制了搭便车行为.由于搭便车节点不提供上传,所以choking以后没有指向搭便车节点的连接,此时,PLX的连接交换机制就能抑制搭便车节点进入文件共享系统.另外,通过对连接交换概率的数学控制,PLX可以区分节点对共享系统的贡献,并根据贡献大小调整其在共享网络中的位置,进一步保证了公平性.最后,对PLX的影响进行了深入的理论分析和模拟实验验证,结果表明:PLX unchoking策略较现有的抵抗搭便车的方法更简单、直接,在效果上有明显提升.展开更多
基金This work was supported by Hebei Province Natural Science Foundation(E2022105032)National Natural Science Foundation of China(51978575,52172359).
文摘Hyperloop has become one of the key reserve technologies for future high-speed rail transit.The gas in the tube is compressed and rubbed,leading to a strong aerodynamic heating effect.The research on the flow field characteristics and aerodynamic heating effect of hyperloop is in its infancy,and that on the flow field structure is lacking.In this study,the nozzle theory was used to make a preliminary judgment on the choked flow phenomenon in the hyperloop.Based on the flow results obtained under different working conditions,the identification basis of the choked flow phenomenon in the hyperloop was obtained.Furthermore,the effect of the choked/unchoked flow on the flow structure,temperature,and pressure distribution of the annular space in the tube was analyzed.Based on traditional high-speed railway aerodynamics,according to relevant theories and calculation in aerospace field,and combined with the model test data,the reliability verification analysis on the characteristics of the flow field are carried out.The structure of the flow filed in the tube can be divided into choked and unchoked.The judgment is dependent on whether the throat reaches the speed of sound.Under the choked flow,a normal shock wave is formed in front of the tube train.The temperature rise of the local flow field exceeds 50 K;the temperature rise of the stagnation region exceeds 88 K,and the pressure is approximately 1.7 times that of the initial pressure in the tube.When the flow is unchoked,differences arise in the distribution of the flow field corresponding to different incoming Mach numbers.When the incoming flow is supersonic,the flow field maintains a supersonic speed,and a bow-shaped shock wave is formed at the front of the tube train.Owing to the shock wave or expansion wave,the local flow field exhibits significant fluctuations in temperature and pressure.Conversely,when the incoming flow is subsonic,the flow field in the tube maintains a subsonic speed,and no shock wave structure is observed.