移动IP技术在VPN中的应用

虚拟专用网络VPN(Virtual Private Networks)是实现在公网上安全传输私有网络信息的一种技术.作为VPN的关键技术之一的隧道技术解决了移动节点的移动性问题.在介绍L2TP与IPSec这2种VPN隧道机制的基础上对它们进行了比较,重点介绍了IPSec在安全性方面的优势,然后介绍了VPN移动用户的问题和VPN的2种隧道模型,最后分析了利用移动IP技术解决VPN中的移动用户问题的优点,并与现有方案VPDN(Virtual Private Dial-up Network)作了比较.     

Driver gas contaminationin a detonation-driven reflected-shock tunnel

A computational study has been carried out to examine the effects of driver gas contamination in the NASA HYPULSE facility at GASL when operating with a detonation driver in reflected-shock tunnel mode. Unlike high-enthalpy shock tunnels which use helium as a driver gas, the driver gas in a detonation driver consists of a mixture of water vapour and argon, which has very different chemical and thermodynamic properties than those of helium. The purpose of the present work is to quantitatively evaluate the effects of driver gas contamination on the flow properties in the test section. Two computational analyses have been performed. The first analysis examined the nozzle flow under the influence of a prescribed level of driver gas contamination. In the second analysis, the transient development of the driver gas leakage in the reflected-shock region in the shock tube is studied. The unique flow features brought about by the detonation-driver gas and the method for detecting the contamination are discussed.Received: 6 August 2002, Revised: 22 September 2003, Published online: 10 February 2004Correspondence to: R.S.M. ChueAn abridged version of this paper was presented at the 23rd International Symposium on Shock Waves at Fort Worth, Texas, July 23 to 27, 2001     

等熵轻质活塞风洞中活塞质量对匹配压力振荡的影响

等熵轻质活塞风洞的管道中被压缩的气体是作为实验段的气源，在实验阶段，要求其压力维持恒值，称此压力为匹配压力，这一条件只有在忽略活塞质量的理想情况下才可实现，本文研究在实际情况下，即考虑活塞质量时，质量对匹配压力振荡的影响，从而得出活塞质量的选择范围。     

基于隧道效应的微机械角速率传感器

提出了一种基于隧道效应的微机械角速率传感器的设计方案,还针对隧穿检测和电容检测进行了比较。并指出基于隧道效应的微机械角速率传感器将极大提高传感器的灵敏度。     

近距侧爆情况下马蹄形隧道动态响应特点的研究

在数值模拟和动光弹试验研究的基础上 ,对马蹄形隧道在邻近爆破作用下的动态响应特点进行了分析 ,并在综合考虑入射应力波波长、隧道直径、爆源与隧道的相对距离的基础上 ,提出了隧道迎爆一侧的动应力集中因子的近似确定方法 ,为今后邻近隧道的爆破施工安全提供了有益的参考。     

Limit Cycle Oscillations of a Wing Section with a Tip Mass

This paper presents an investigation into the limit cycleoscillation phenomenon for a nonlinear aeroelasticsystem under unsteady aerodynamics. The system consists of a sweptbackwing section carrying a tip mass with one degree of freedom. Thejunction stiffness considered between the wing and the tip mass istrilinear. The method of harmonic balance, which can be very practicalin the study of nonlinear flutter, is used for the theoretical analysisof limit cycle oscillations. Stable, unstable and semi-stable limitcycles are predicted in the system for both cases of hardening andsoftening springs. Results found by numerical simulation provide theamplitudes of limit cycles. The experimental results in wind tunneltests agree well with the predictions obtained both theoretically andnumerically.     

围岩流变特性对隧道二衬支护时机的影响

为了研究岩体流变特性情况下隧道二衬的支护时机,首先推导了在考虑围岩流变特性时,衬砌抗力、位移及围岩的位移表达式;然后以广梧高速公路茶林顶隧道岩体为工程背景,探讨了考虑岩体流变情况下,隧道二衬支护时机的确定方法,并对比了围岩拱顶下沉实测值和理论计算值。结果表明：(1) 理论分析所建立的衬砌抗力、位移及围岩的位移表达式中均包含了时间参数,可确定达到不同衬砌抗力、位移及围岩位移所需要的时间;(2) 围岩拱顶下沉实测值和理论计算值表现出相同的发展规律,验证了所建立方法的正确性。     

隧道健康动态评价模型与应用

在隧道健康安全评价的指标体系及其等级标准的基础上,通过规范化处理样本资料库中的元素,消除了指标类型和量纲的影响后,提出用集对分析方法构造可变模糊集的相对差异度函数,合理的确定了各层相关隧道健康评价指标处于级别标准区间的相对隶属函数,采用乘积标度法确定相关指标权重后,得出了隧道健康模糊综合评价动态模型。确定健康级别指标特征值后,结合实例计算证明了文中所提方法的科学性与合理性,有利于推动可变模糊集理论在土木工程领域的进一步发展。     

盾构隧道下穿输水干渠设计参数优化模型试验

盾构隧道下穿输水干渠设计参数(最优夹角、最小埋深)对隧道路线选择、干渠扰动影响评价至关重要,现行规范尚无明确规定。随着盾构施工技术成熟,有必要深入研究盾构隧道下穿输水干渠的最优夹角与最小埋深参数。依托郑州地铁10号线下穿南水北调干渠工程,基于Buckingham-π定律推导的相似参数,开展盾构隧道下穿输水干渠设计参数优化室内相似模型试验。研究结果表明：(1)隧道轴线与渠坡底部相交的局部区域地层沉降量大于周围地层沉降量;(2)当采用朗肯土压力计算值作为盾构仓压值,盾构隧道埋深不宜小于1.5D,夹角不得小于30°;(3)考虑盾构隧道施工对渠表的影响,应优先考虑隧道埋深的扰动影响,其次考虑隧道夹角设计参数的扰动影响。试验结果将为盾构隧道下穿输水干渠设计参数提供了重要参考依据。     

Upstream porthole injection in a 2-D scramjet model

Injection from portholes upstream of the combustion chamber was investigated as a method of delivering fuel into a scramjet. This method reduces the viscous drag on a model by allowing a reduction in the length of the combustion chamber. At experimental enthalpies of 3.0 MJ/kg in the T4 shock tunnel, there was no evidence of combustion in the intake, either by shadowgraph or pressure measurements. Combustion was observed in the combustion chamber. A theoretical extension of these results is made to a hot wall scenario. Received 2 January 2001 / Accepted 3 August 2001