射弹撞击带盖炸药引发爆轰的机制

进行了钢射弹引爆带厚盖板的Ｔ／Ｒ（４／６）炸药的实验，观测了炸药中引发的爆轰波阵面波形。有两种结构的盖板：一种是整体钢盖板，另一种是预制塞钢盖板。在略大于引爆阈值的撞击条件下，覆盖整体盖板的炸药中出现凸面爆轰波，而在覆盖预制塞盖板的炸药中出现Ｗ形爆轰波。这一现象表明，冲击效应是前者引发爆轰的主控机制，而宏观剪切效应是后者引发爆轰的主控机制。按冲击引爆和剪切引爆机制分别进行了射弹引爆带整体盖板和预制     

水中爆炸冲击波测试技术研究

改进锰铜压力计，ＰＶＤＦ压力计算测试系统，并用该系统进行实验研究，得到了ＴＮＴ／ＲＤＸ＝４０／６０炸药球水国爆炸冲击波在１≤Ｒ／Ｒ０≤１２０范围内的峰值压力随距离的衰减规律。     

一类非线性离散人口模型的稳定性和振动性

本文讨论了非线性差分方程ｘｎ＋１＝ｘｎ／１－ａ－ｂｘｎ－ｋ＋ｃｘ＾２ｎ－ｋ平衡点的稳定性，并获得了此方程在条件ａ∈（１，∞），ｂ∈（－∞，＋∞）＝Ｒ，ｃ∈（０，∞）下其正解的渐近性质及其关于正平衡点振动的充分条件，且当Ｋ＝０时建立了正平衡点渐近稳定的充分必要性准则。’     

Modal part analysis of slosh of the liquid in a cylindrical container in the case of small bond number

ＩｎｔｒｏｄｕｃｔｉｏｎＴｈｅｍｏｔｉｏｎｏｆｔｈｅｉｎｖｉｓｃｉｄ,ｉｒｒｏｔａｔｉｏｎａｌａｎｄｉｎｃｏｍｐｒｅｓｓｉｂｌｅｆｌｕｉｄｉｎａｃｙｌｉｎｄｒｉｃａｌｃｏｎｔａｉｎｅｒｗｉｔｈｒａｄｉｕｓａｉｓｇｏｖｅｒｎｅｄｂｙＦｉｇ．１Ｓｌｏｓｈｏｆａｌｉｑｕｉｄｉｎａｃｙｌｉｎｄｒｉｃａｌｃｏｎｔａｉｎｅｒ２＝０　　（ｉｎＶ）,（１）ｒ＝０　　（ｏｎｒ＝ａ）,（２）ｚ＝０　　（ｏｎｚ＝－ｈ）,（３）ηｔ＋·η＝ｚ　　（ｏｎｚ＝η）,（４）ｔ＋１２｜…     

PERIODIC SOLUTIONS OF A CLASS OF HIGHER ORDER NEUTRAL TYPE EQUATIONS

ＩｎｔｒｏｄｕｃｔｉｏｎＩｎｔｈｉｓｐａｐｅｒ,ｗｅｃｏｎｓｉｄｅｒｐｅｒｉｏｄｉｃｓｏｌｕｔｉｏｎｐｒｏｂｌｅｍｏｆｈｉｇｈｅｒｏｒｄｅｒｎｅｕｔｒａｌｔｙｐｅｅｑｕａｔｉｏｎｏｆｔｈｅｆｏｒｍｘ（ｋ）（ｔ）＋∑ｋｉ＝１ａｉｘ（ｋ－ｉ）（ｔ）＋∑ｋ...     

输沙量（率）水平分布的非均一性

实验表明：输沙率沿风洞实验段横截面的水平分布具有明显的非均一性。其正负距平变幅可达平均值的４５－６０％。输沙率与有效起沙风成正比关系，其实验式为ｑ＝８．９５×１０（－１）（ＶＬ－Ｖｔ）（１．９）（ｇ／ｃｍ·ｍｉｎ），Ｖｔ＝５．０ｍ／ｓ。与Ｂａｇｎｏｌｄ，ＲＡ理论公式ｑ＝８．７０×１０（－２）（Ｖ－Ｖｔ）３相比（Ｖｔ＝４．０ｍ／ｓ），前者计算结果更接近室内外实测值。     

A complete expression of the asymptotic solution of differential equation with three-turning points

Ｗｅｈａｖｅｄｉｓｃｕｓｓｅｄｃｏｎｃｅｐｔｏｆｅｑｕａｔｉｏｎｗｉｔｈｎ＿ｔｕｒｎｉｎｇｐｏｉｎｔｓｉｎｍｙｐａｐｅｒ［１］,ｉ．ｅ．,ａｓｅｃｏｎｄｏｒｄｅｒｌｉｎｅａｒｏｒｄｉｎａｒｙｄｉｆｆｅｒｅｎｔｉａｌｅｑｕａｔｉｏｎｄ２ｙｄｘ２＋［λ２ｑ１（ｘ）＋λｑ２（ｘ,λ）］ｙ＝０,ｗｈｅｒｅｑ１（ｘ）＝（ｘ－μ１）（ｘ－μ２）…（ｘ－μｎ）ｆ（ｘ）,ｆ（ｘ）≠０,ａｎｄλｉｓａｌａｒｇｅｐａｒａｍｅｔｅｒ．Ａｌｔｈｒｏｕｇｈｔｈｅｆｉｒｓｔｔｅｒｍｏｆｔｈｅａｓｙｍｐｔｏｔｉｃｅｘｐａｎ…     

A novel solution of toroidal shells under axisymmetric loading

μ＝ｒ０／Ｒ０,κ＝１２（１－ν２）μｒ０／ｈ,λ２＝ｉκ,ν—Ｐｏｉｓｏｎ’ｓｒａｔｉｏ,θ—ｔａｎｇｅｎｔｉａｌａｎｇｌｅｏｆｓｈｅｌ,ｒ０—ｒａｄｉｕｓｏｆｔｈｅｍｅｒｉｄｉａｎｃｉｒｃｌｅ,ｈ—ｗａｌｔｈｉｃｋｎｅｓｏｆｓｈｅｌｓ,ｃｏｎｓｔ...     

《小问题》上期解答

《小问题》上期解答答２８７．１．Ｊｃ＝Ｊ０－ｍｌ２＝１２－１６９π２ｍｒ２，本题为单自由度，取广义坐标θ．粗糙时：速度瞬心为Ｐ１，ＪＰ１＝Ｊｃ＋ｍＣＰ１２＝３２－８３πｃｏｓθｍｒ２．动能Ｔ＝１２ＪＰ１θ２＝１２３２－８３πｃｏｓθｍｒ２θ２．图３图...     

《小问题》上期解答

《小问题》上期解答答２８７．１．Ｊｃ＝Ｊ０－ｍｌ２＝１２－１６９π２ｍｒ２,本题为单自由度,取广义坐标θ．粗糙时：速度瞬心为Ｐ１,ＪＰ１＝Ｊｃ＋ｍＣＰ１２＝３２－８３πｃｏｓθｍｒ２．动能Ｔ＝１２ＪＰ１θ２＝１２３２－８３πｃｏｓθｍｒ２θ２．图３图...     

Preface

This special issue of PARTICUOLOGY is devoted to the first UK-China Particle Technology Forum taking place in Leeds, UK, on 1-3 April 2007. The forum was initiated by a number of UK and Chinese leading academics and organised by the University of Leeds in collaboration with Chinese Society of Particuology, Particle Technology Subject Group （PTSG） of the Institution of Chemical Engineers （IChemE）, Particle Characterisation Interest Group （PCIG） of the Royal Society of Chemistry （RSC） and International Fine Particle Research Institute （IFPRI）. The forum was supported financially by the Engineering and Physics Sciences Research Council （EPSRC） of United Kingdom,     

The 7th International Conference on Fluid Mechanics May 24-27,2015,Qingdao,China

正http://www.icfm7.org First Announcement and Call for PapersThe objective of International Conference on Fluid Mechanics(ICFM)is to provide a forum for researchers to exchange new ideas and recent advances in the fields of theoretical,experimental,computational Fluid Mechanics as well as interdisciplinary subjects.It was successfully convened by the Chinese Society of Theoretical and Applied Mechanics(CSTAM)in Beijing(1987,     

INFORMATION FOR CONTRIBUTORS

Contributions： The Journal, Acta Mechanica Solida Sinica, is pleased to receive papers from engineers and scientists working in various aspects of solid mechanics. All contributions are subject to critical review prior to acceptance and publication.     

Guide for authors

正Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica Sinica.     

基于鲁棒滤波的捷联导引头视线角速度估计方法

针对捷联导引头无法直接获取视线角速度等信息的问题,研究了鲁棒滤波在大气层外飞行器捷联导引头视线角速度估计中的应用。为了建立非线性滤波估计模型,考虑目标视线角速度的慢变特性,采用一阶马尔科夫模型建立了状态方程;推导了视线角速度的解耦模型,并建立了量测方程;考虑到实际应用中存在系统噪声统计特性失准的问题,基于Huber-Based鲁棒滤波方法,设计了视线角速度滤波器,并完成了基于Huber-Based滤波方法和扩展卡尔曼滤波方法的数学仿真。仿真结果表明Huber-Based滤波方法的视线角、视线角速度及视线角加速度估计精度分别达到0.1140'、0.1423'/s、0.0203'/s2,而扩展卡尔曼滤波方法的视线角、视线角速度及视线角加速度估计精度仅分别为0.6577'、0.6415'/s、0.0979'/s~2。仿真结果证明了该方法可以有效地估计出相对视线角速度等信息,并且在非高斯噪声的条件下,依然可获得较高的估计精度,具有一定的鲁棒性。     

Guide for authors

正Each of the sections below provides essential information for authors.We recommend that you take the time to read them before submitting a contribution to Acta Mechanica Sinica.We hope our guide to authors may help you navigate to the appropriate section.How to prepare a submission This document provides an outline of the editorial process involved in publishing a scientific paper in Acta Mechanica