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排序方式: 共有1125条查询结果,搜索用时 312 毫秒
901.
波长共享的WDM无源光网络媒质接入控制算法及其性能分析 总被引:2,自引:2,他引:0
结合波长分配和前跳虚时钟算法,提出了一个基于连接的WDM无源光网络媒质接入控制算法.通过理论和仿真,分析了此算法的延时保证和公平性. 相似文献
902.
基于100 m色散位移光纤的超连续谱实验研究 总被引:2,自引:1,他引:1
利用被动锁模掺铒光纤激光器输出的重复频率13.9 MHz、中心波长1557.28 nm的光脉冲作泵浦源,在100 m的色散位移光纤中产生总宽度达488 nm的超连续谱,不平坦度小于±3.0 dB,利用法布里-珀罗滤波器获得163路多波长脉冲,利用可调谐滤波器得到C波段内脉宽为1.2~2.0 ps的近变换限超短光脉冲.分析了泵浦脉冲的功率、光纤长度等因素对SC光谱展宽的作用,并与色散平坦光纤和较长的色散位移光纤作了比较. 相似文献
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基于相位补偿的BPSK相参脉冲串信号多普勒频率变化率估计算法 总被引:1,自引:0,他引:1
目标与观测平台之间径向加速度引起的接收信号多普勒频率变化率的精确估计对于高精度单站无源定位与跟踪具有重要意义。该文针对脉内相位调制信号的频率变化率不能直接表征多普勒频率变化率的问题,首先引入相位补偿的方法消除BPSK相位调制序列的影响,然后针对固定脉冲重复频率和脉冲重复频率抖动两种情况分别提出了径向加速度引起的多普勒频率变化率的精确估计方法,并且给出了多普勒频率变化率与采样频率、观测时间及脉冲重复频率之间的约束关系。仿真结果表明,典型参数条件下该文提出算法的信噪比门限比已有算法低约4~6 dB。 相似文献
906.
Shock formation due to flow compressibility and its interaction with boundary layers has adverse effects on aerodynamic characteristics, such as drag increase and flow separation. The objective of this paper is to appraise the prac-ticability of weakening shock waves and, hence, reducing the wave drag in transonic flight regime using a two-dimensional jagged wall and thereby to gain an appropriate jagged wall shape for future empirical study. Different shapes of the jagged wall, including rectangular, circular, and triangular shapes, were employed. The numerical method was validated by experimental and numerical studies involving transonic flow over the NACA0012 airfoil, and the results presented here closely match previous experimental and numerical results. The impact of parameters, including shape and the length-to-spacing ratio of a jagged wall, was studied on aerodynamic forces and flow field. The results revealed that applying a jagged wall method on the upper surface of an airfoil changes the shock structure significantly and disinte-grates it, which in turn leads to a decrease in wave drag. It was also found that the maximum drag coefficient decrease of around 17%occurs with a triangular shape, while the max-imum increase in aerodynamic efficiency (lift-to-drag ratio) of around 10%happens with a rectangular shape at an angle of attack of 2.26?. 相似文献
907.
Jaekwon Ko Hwanseong Jeong Sun Young Choi Fabian Rotermund Dong-Il Yeom Byoung Yoon Kim 《Current Applied Physics》2017,17(1):37-40
We demonstrated four different laser operational states in the same passive fiber ring laser cavity by controlling solely the polarization state in a saturable absorber. The demonstrated laser operational states were continuous wave, mode-locking, Q-switching, and Q-switched mode-locking. The saturable absorber was fabricated by spin-coating a single-walled carbon nanotubes (SWCNT)/polymer composite on a side polished fiber providing enhanced nonlinear interaction with the SWCNT. The wide tuning range of the saturable absorber allows the simple means to generate different forms of laser output from a single laser cavity. 相似文献
908.
微波辐射亮温图像的模拟在被动遥感领域中具有重要意义。该文根据射线追踪的思想提出了一种三维场景微波辐射图像的模拟方法:亮温追踪法。分析了模拟时必须考虑的天空背景辐射、多次反射造成的极化旋转以及天线平滑作用等影响因素,最终建立了微波辐射亮温图像的模拟方法。应用此方法对典型目标进行了试验模拟,并对模拟结果所表现出的微波辐射现象进行了分析。为验证模拟方法的可靠性,该文对楼层建筑以及飞机跑道等实际场景进行模拟,模拟结果与实地测量图像取得了很好的一致,表明此方法完全可行。 相似文献
909.
Understanding how to decrease the friction drag exerted by a fluid on a solid surface is becoming increasingly important to address key societal challenges, such as decreasing the carbon footprint of transport. Well-established techniques are not yet available for friction drag reduction. Direct numerical simulation results obtained by Józsa et al. (2019) previously indicated that a passive compliant wall can decrease friction drag by sustaining the drag reduction mechanism of an active control strategy. The proposed compliant wall is driven by wall shear stress fluctuations and responds with streamwise wall velocity fluctuations. The present study aims to clarify the underlying physical mechanism enabling the drag reduction of these active and passive control techniques. Analysis of turbulence statistics and flow fields reveals that both compliant wall and active control amplify streamwise velocity streaks in the viscous sublayer. By doing so, these control methods counteract dominant spanwise vorticity fluctuations in the near-wall region. The lowered vorticity fluctuations lead to an overall weakening of vortical structures which then mitigates momentum transfer and results in lower friction drag. These results might underpin the further development and practical implementation of these control strategies. 相似文献
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