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Effect of local wall temperature on hypersonic boundary layer stability and transition
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作者 鲁锐洋 黄章峰 《Chinese Physics B》 SCIE EI CAS CSCD 2023年第11期508-517,共10页
Wall temperature significantly affects stability and receptivity of the boundary layer. Changing the wall temperature locally may therefore be an effective laminar flow control technique. However, the situation is com... Wall temperature significantly affects stability and receptivity of the boundary layer. Changing the wall temperature locally may therefore be an effective laminar flow control technique. However, the situation is complicated when the wall temperature distribution is nonuniform, and researchers have experimentally found that local wall cooling may delay the onset of transition. We attempt to clarify the physical mechanisms whereby the local wall temperature affects the transition and the stability of a hypersonic boundary layer. A numerical investigation of the disturbance evolution in a Mach-6 sharp cone boundary layer with local wall heating or cooling is conducted. Direct numerical simulation(DNS) is performed for the single-frequency and broadband disturbance evolution caused by random forcing. We vary the local wall temperature and the location of heating/cooling, and then use the eNmethod to estimate the transition onset. Our results show that local wall cooling amplifies high-frequency unstable waves while stabilizing low-frequency unstable waves, with local heating amplifying all unstable waves locally. The disturbance amplitude and second-mode peak frequency obtained by DNS agree well with the previous experimental results. Local cooling/heating has a dual effect on the stability of the hypersonic boundary layer. For local cooling, while it effectively inhibits the growth of the low-frequency unstable waves that dominate the transition downstream, it also further destabilizes the downstream flow. In addition, while upstream cooling can delay the transition, excessive cooling may promote it;local heating always slightly promotes the transition.Finally, recommendations are given for practical engineering applications based on the present results. 展开更多
关键词 hypersonic boundary layers direct numerical simulations linear stability theory
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Linear stability theory with the equivalent spanwise wavenumber correction in 3D boundary layers
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作者 Runjie SONG Shaolong ZHANG Jianxin LIU 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI CSCD 2019年第3期407-420,共14页
The prediction on small disturbance propagation in complex three-dimensional(3D) boundary layers is of great significance in transition prediction methodology, especially in the aircraft design. In this paper, the lin... The prediction on small disturbance propagation in complex three-dimensional(3D) boundary layers is of great significance in transition prediction methodology, especially in the aircraft design. In this paper, the linear stability theory(LST) with the equivalent spanwise wavenumber correction(ESWC) is proposed in order to accurately predict the linear evolution of a disturbance in a kind of boundary layer flow with a vital variation in the spanwise direction. The LST with the ESWC takes not only the scale of the mean flow with the significant variation but also the wavenumber evolution of the disturbance itself. Compared with the conventional LST, the results obtained by the new method are in excellent agreement with those of the numerical simulations. The LST with the ESWC is an effective method on the prediction of the disturbance evolution in 3D boundary layers, which improves the prediction of the LST in the applications to complex 3D boundary layers greatly. 展开更多
关键词 three-dimensional(3D)boundary layer prediction of DISTURBANCE propagation EQUIVALENT spanwise WAVENUMBER LINEAR stability theory(LST) numerical simulation
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Theoretical investigation on shocklets in compressible boundary layers
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作者 袁湘江 刘智勇 +1 位作者 沈清 李国良 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2014年第8期935-946,共12页
By the shock relationships, the wavy characteristics and the forming condi-tions of a shock wave are analyzed. The wavy characteristics of an Euler system are stud-ied theoretically. The present research focuses on th... By the shock relationships, the wavy characteristics and the forming condi-tions of a shock wave are analyzed. The wavy characteristics of an Euler system are stud-ied theoretically. The present research focuses on the wavy characteristics of Tollmien-Schlichting (T-S) waves, the excitation conditions of shocklets in compressible boundary layers, and the viscous effect on shock. The possibility of existence of shocklets in the compressible boundary layer and the physical mechanism of formation are theoretically interpreted. 展开更多
关键词 wave theory SHOCKLET boundary layer Tollmien-Schlichting (T-S) wave
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ON THE MECHANISM OF TURBULENT COHERENT STRUCTURE(II)──A PHYSICAL MODEL OF COHERENT STRUCTURE FOR THE ROUGH BOUNDARY LAYER
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作者 刘宇陆 蔡树棠 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 1996年第3期197-203,共7页
In this paper, the differences of turbulent coherent structure beween the smooth and rough boundary lavers are analysed.Based on the discussing the transient properties from the smooth wall tothe rough wall,the physic... In this paper, the differences of turbulent coherent structure beween the smooth and rough boundary lavers are analysed.Based on the discussing the transient properties from the smooth wall tothe rough wall,the physicalmodel of coherent structure for the rough boundary layer are established.The width of slwly-moving turbulent spot and the bursting time are obtained,which are in agreement with experimental results. 展开更多
关键词 turbulent theory coherent structure rough boundary layer
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微通道换热器拓扑结构优化与性能研究
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作者 陈彦松 阮达 +3 位作者 刘渊博 郑通 张帅帅 马学虎 《化工学报》 EI CSCD 北大核心 2024年第3期823-835,共13页
换热器结构拓扑优化可将传热强化设计问题转化为数学优化问题进行求解,对于设计新颖高效换热器具有重要价值。然而,拓扑优化数学模型难以直接解释优化结果的几何特征及相应强化机理。以传热量为目标,对微通道换热器进行拓扑优化设计,研... 换热器结构拓扑优化可将传热强化设计问题转化为数学优化问题进行求解,对于设计新颖高效换热器具有重要价值。然而,拓扑优化数学模型难以直接解释优化结果的几何特征及相应强化机理。以传热量为目标,对微通道换热器进行拓扑优化设计,研究了不同参数对换热器强化结构特征和换热器性能的影响。结果表明,拓扑优化换热器的通道结构呈现多级分叉构型,分叉的数量随着入口Reynolds数、翅片传热效率和流体Prandtl数的增大而增多。在此基础上,采用耗散和边界层理论分析了拓扑优化分叉通道与流体边界层厚度的内在联系,为换热器结构强化设计提供了新的思路。 展开更多
关键词 优化设计 微通道 传递过程 分级通道结构 边界层理论
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Gao's interacting shear flows( ISF) theory and its inferences and their applications 被引量:1
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作者 于勇 张海荣 《Journal of Beijing Institute of Technology》 EI CAS 2013年第3期291-300,共10页
Gao's viscous/in-viscid interacting shear flows (ISF) theory, proposed by professor Gao Zhi in Institute of Mechanics, China Academy of Science, and its inferences and their applications in computational fluid dyna... Gao's viscous/in-viscid interacting shear flows (ISF) theory, proposed by professor Gao Zhi in Institute of Mechanics, China Academy of Science, and its inferences and their applications in computational fluid dynamics (CFD) are reviewed and some subjects worthy to be studied are pro- posed in this paper. The flow-field and motion law of ISF, mathematics definition of strong viscous shear layer flow in ISF, ISF equations, wall-surface compatibility criteria (Gao's criteria ), space scale variety law of strong viscous shear layer reveals flow mechanism and local space small scale triggered by strong interaction that cause some abnormal severe local pneumatic heating phenomenon in hypersonic flow. Gao's ISF theory was used in near wall flow, free ISF flow simulation and design of computing grids, Gao's wall-surface criteria were used to verify calculation reliability and accuracy of near wall flows, ISF theory approximate analytical result of shock waves-boundary layer interac- tion and ISF equations were used to obtain the numerical exact solution of local area flow ( such as stationary point flow). Some new subjects, such as, improving near-wall turbulent models according to the turbulent flow simulation satisfying the wall-criteria and illustrating relation between grid-con- vergence based on the wall criteria and other convergence tactics, are suggested. The necessity of applying Gao's ISF theory and wall criteria is revealed. Difficulties and importance of hypersonic vis- cous/in-viscid interaction phenomenon were also emphasized. 展开更多
关键词 viscous/in-viscid interaction shear flow (ISF) theory shock wave-boundary layer inter-action hypersonic flow computational fluid dynamics (CFD)
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A Statistical Rate Theory of Interface Concentration during Solution ZeoliteCrystal Growth
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作者 Hongwei Song Olusegun J. Ilegbusi 《Journal of Crystallization Process and Technology》 2011年第3期33-40,共8页
A theoretical model is developed using statistical rate theory to determine the rate of molecular transport across the interface of a growing spherical zeolite crystal. The model is expressed in terms of the interface... A theoretical model is developed using statistical rate theory to determine the rate of molecular transport across the interface of a growing spherical zeolite crystal. The model is expressed in terms of the interface concentration. Two model constants appear in the expression for the equilibrium exchange rate. In order to validate the model, zeolite crystallization is investigated for a system for which experimental data exist. The model constants were first established using the measured growth rates at a specific temperature. Then the model was used to predict the growth rate at other temperatures. 展开更多
关键词 ZEOLITE CRYSTAL Growth STATISTICAL Rate theory boundary layer MICROGRAVITY
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一种数据驱动的气动热预示模型 被引量:2
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作者 王泽 王梓伊 +2 位作者 王旭 宋述芳 张伟伟 《空气动力学学报》 CSCD 北大核心 2023年第5期12-19,I0001,共9页
高效、高精度的气动热预示是高超声速飞行器设计的关键。然而,随着高超声速飞行器外形的日益复杂化和设计周期的不断缩紧,现有方法已很难满足高效精准的气动热预示。本文基于边界层理论和支持向量机发展了一种数据驱动的当地化气动热预... 高效、高精度的气动热预示是高超声速飞行器设计的关键。然而,随着高超声速飞行器外形的日益复杂化和设计周期的不断缩紧,现有方法已很难满足高效精准的气动热预示。本文基于边界层理论和支持向量机发展了一种数据驱动的当地化气动热预示建模方法。首先,通过求解Euler方程获得边界层外缘信息,采用RANS方法计算热流分布样本;然后,通过设计的特征选择方法确定边界层外缘特征;最后,利用支持向量机构建气动热预示模型,实现边界层外缘特征与壁面热流的映射。对双椭球和二级压缩面的热流预示结果表明,该模型考虑了非均匀分布壁面温度等边界条件,具有较高的预示精度和良好的外推与泛化性能,典型位置热流预示结果和RANS计算结果的相对误差均小于5%。同时,以双椭球上表面中心线热流预示为例,对比传统POD降阶方法,发现该模型的预示精度更高,外推状态下预示精度较POD方法提升了4倍以上。 展开更多
关键词 气动热 边界层理论 支持向量机 特征选择 当地化模型
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声学超表面抑制高速边界层内宽频不稳定模态研究 被引量:1
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作者 王蔚彰 孔维萱 +1 位作者 严昊 赵瑞 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2023年第2期388-396,共9页
以声学超表面为研究对象,使用线性稳定性理论(LST),研究了声学超表面导纳相位与幅值对超声速平板边界层内宽频不稳定模态的影响规律。结果表明:当导纳相位θ接近0.5π时,第1模态被抑制的同时第2模态会被激发,且在较低频率范围内导纳幅... 以声学超表面为研究对象,使用线性稳定性理论(LST),研究了声学超表面导纳相位与幅值对超声速平板边界层内宽频不稳定模态的影响规律。结果表明:当导纳相位θ接近0.5π时,第1模态被抑制的同时第2模态会被激发,且在较低频率范围内导纳幅值的增大能够使第1模态更加稳定;当导纳相位θ接近π时,可抑制第2模态但同时激发第1模态;整体上,导纳幅值越大,对不稳定模态的抑制或激发效果越明显。在此基础上,结合缝隙几何参数对导纳的影响,提出一种可实现性宽频抑制方案,通过分段设计声学超表面微结构的几何尺寸,实现了同时抑制第1模态和高频第2模态的目标,并使用eN方法验证了转捩抑制效果。 展开更多
关键词 声学超表面 不稳定模态 线性稳定性分析 边界层转捩 超声速流动
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变热导率的幂律流体在水平波面上的传热问题研究
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作者 刘芳芳 张爱莉 +1 位作者 司新辉 曹丽梅 《工程科学学报》 EI CSCD 北大核心 2023年第11期1977-1984,共8页
根据泰勒展开式和边界层理论,推导了变热导率的Oswad-de Waele幂律流体沿水平波面上的边界层方程.假设热传导系数是依赖于温度梯度的幂律函数,构建了变热导率的能量方程模型.引入一系列变换,把变量量纲为一化和坐标变换,将原始问题转换... 根据泰勒展开式和边界层理论,推导了变热导率的Oswad-de Waele幂律流体沿水平波面上的边界层方程.假设热传导系数是依赖于温度梯度的幂律函数,构建了变热导率的能量方程模型.引入一系列变换,把变量量纲为一化和坐标变换,将原始问题转换为偏微分方程组,并用Keller-box方法进行数值求解.讨论了某些参数如波幅与波长的比值、幂律指数以及广义普朗特数对壁面摩擦和流体传热的影响.计算结果显示:表面速度和压力梯度沿波面呈周期性变化,而且它们的变化周期与波面的变化周期完全一致.而对于壁面的摩擦系数和局部Nusselt数,在靠近零点的地方会有剧烈震荡,沿轴向会呈现波形分布状态,随着波长比率的增大而减小,且会随着振幅的增大,壁面摩擦系数也会震荡加剧.随着幂律指数的增加,局部Nusselt数呈现递减的分布状态.对于问题的特殊情况,当壁面是光滑平板时,尽管壁面的摩擦系数和局部Nusselt数沿轴向在初始位置会有波动,但会在很短的距离达到稳定的状态.从不同参数对周期的影响来看,周期性波动的壁面摩擦系数和局部Nusselt数与波面曲线的峰顶和波谷并不保持一致. 展开更多
关键词 幂律流体 正弦波面 变热导率 泰勒展式 边界层理论
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泡沫碳表面对高超声速边界层稳定性影响
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作者 王蔚彰 赵瑞 +2 位作者 桂裕腾 吴杰 涂国华 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2023年第10期2741-2749,共9页
高超声速边界层转捩会使壁面摩阻和热流显著增加,严重影响飞行器的性能。微孔隙表面在不明显改变平均流场的同时,能够有效抑制边界层转捩,具有较大的应用潜力。在马赫数为6的Ludwieg管风洞中研究泡沫碳孔隙材料对尖锥边界层中不稳定波... 高超声速边界层转捩会使壁面摩阻和热流显著增加,严重影响飞行器的性能。微孔隙表面在不明显改变平均流场的同时,能够有效抑制边界层转捩,具有较大的应用潜力。在马赫数为6的Ludwieg管风洞中研究泡沫碳孔隙材料对尖锥边界层中不稳定波的影响规律,试验结果表明:尖锥边界层存在明显的第2模态波,其特征频率随着流向位置增加而减小。相比于光滑表面,泡沫碳表面使不同流向位置上的第2模态波增长率均有明显下降,至少延长第2模态传播区域21.6%。此外,采用阻抗管测量泡沫碳表面的声学特性获取阻抗模型系数,并结合线性稳定性理论预测了泡沫碳表面扰动模态增长率,理论结果与试验结果变化趋势相同。 展开更多
关键词 边界层稳定性 微孔隙表面 高超声速 风洞试验 线性稳定性理论
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边界层对粗糙单裂隙溶质运移影响试验
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作者 田峥颖 陈舟 +2 位作者 马兴 杜昭颖 金敏 《河海大学学报(自然科学版)》 CAS CSCD 北大核心 2023年第2期106-113,共8页
为探究非费克(non-Fickian)运移表现出的峰值提前到达和拖尾等现象,开展了粗糙单裂隙溶质运移试验,总结了粗糙单裂隙中溶质运移特征及运移机理,结合边界层理论对峰值提前到达和拖尾现象进行了分析和解释。结果表明:峰值时间和拖尾时间... 为探究非费克(non-Fickian)运移表现出的峰值提前到达和拖尾等现象,开展了粗糙单裂隙溶质运移试验,总结了粗糙单裂隙中溶质运移特征及运移机理,结合边界层理论对峰值提前到达和拖尾现象进行了分析和解释。结果表明:峰值时间和拖尾时间与边界层厚度之间存在较好的线性相关关系;边界层对裂隙介质溶质运移有较为显著影响,即水流速度越小,边界层厚度越大,滞留在边界层内部的溶质越多,溶质获取率越低;粗糙单裂隙中溶质穿透曲线的峰值提前和拖尾现象是由裂隙中心处以惯性力主导的主流区和裂隙壁面以黏性力主导的边界层区共同作用造成的,其中峰值时间主要由主流区的对流因素控制,而边界层区域的存在对拖尾时间影响较大。 展开更多
关键词 溶质运移 非费克运移 峰值时间 拖尾时间 边界层理论 粗糙单裂隙
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e^(N)方法用于高超声速圆锥边界层转捩预测的可靠性 被引量:1
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作者 杨潇楠 苏彩虹 《气体物理》 2023年第2期44-55,共12页
e^(N)方法基于扰动在边界层中线性演化过程中的幅值增长程度来预测转捩。以来流Mach数为6、不同壁面温度条件下不同钝度圆锥为研究对象,结合直接数值模拟和抛物化稳定性方程,从e^(N)方法是否能够准确描述扰动在上述边界层中线性增长的角... e^(N)方法基于扰动在边界层中线性演化过程中的幅值增长程度来预测转捩。以来流Mach数为6、不同壁面温度条件下不同钝度圆锥为研究对象,结合直接数值模拟和抛物化稳定性方程,从e^(N)方法是否能够准确描述扰动在上述边界层中线性增长的角度,分析了该方法预测转捩的可靠性。研究结果表明,在小钝度或高壁面温度情况下,扰动在向下游的演化过程中从第1模态转变为第2模态,基于线性稳定性理论的e^(N)方法变得不再可靠。壁面温度相同,头部钝度越大,e^(N)方法越可靠;同等钝度下,壁面温度越低,e^(N)方法越可靠。由于存在模态转换时,线性稳定性理论总是低估扰动的增长,因而对于给定的转捩判据N_(T)(可由某一工况实验标定给出),若钝度减小或壁面温度增加到一定程度,e^(N)方法给出的转捩位置比实际情况更靠后。重新标定转捩判据时,钝度越小,壁面温度越高,N_(T)的修正程度就越大。 展开更多
关键词 高超声速 边界层 线性稳定性理论 转捩预测 e^(N)方法
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Physical implication of two problems in transition prediction of boundary layers based on linear stability theory 被引量:5
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作者 SU CaiHong 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2014年第5期950-962,共13页
Up to now,the most widely used method for transition prediction is the one based on linear stability theory.When it is applied to three-dimensional boundary layers,one has to choose the direction,or path,along which t... Up to now,the most widely used method for transition prediction is the one based on linear stability theory.When it is applied to three-dimensional boundary layers,one has to choose the direction,or path,along which the growth rate of the disturbance is to be integrated.The direction given by using saddle point method in the theory of complex variable function is seen as mathematically most reasonable.However,unlike the saddle point method applied to water waves,here its physical meaning is not so obvious,as the frequency and wave number may be complex.And on some occasions,in advancing the integration of the growth rate of the disturbance,up to a certain location,one may not be able to continue the integration,because the condition for specifying the direction set by the saddle point method can no longer be satisfied on the basis of continuously varying wave number.In this paper,these two problems are discussed,and suggestions for how to do transition prediction under the latter condition are provided. 展开更多
关键词 线性稳定性理论 物理意义 边界层 预测 转捩 复变函数 连续变化 增长率
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基于聚合跟踪误差的多USV自适应连续协调控制
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作者 张爱华 宋季强 +1 位作者 张洁 杨凌耀 《测控技术》 2023年第10期82-88,共7页
针对仅邻近多无人水面船(Unmanned Surface Vessel, USV)在无向连通通信拓扑结构下,USV协调轨迹跟踪控制问题,提出一种基于领航者跟随协调策略的分布式自适应连续跟踪控制算法。通过引入虚拟领航者,假设其已知期望轨迹和期望速度,利用... 针对仅邻近多无人水面船(Unmanned Surface Vessel, USV)在无向连通通信拓扑结构下,USV协调轨迹跟踪控制问题,提出一种基于领航者跟随协调策略的分布式自适应连续跟踪控制算法。通过引入虚拟领航者,假设其已知期望轨迹和期望速度,利用跟随者的队形位置跟踪误差和速度跟踪误差构造聚合跟踪误差。进而基于协调跟踪控制系统的聚合跟踪误差系统模型,使用自适应项补偿外界环境的干扰,结合边界层理论提出分布式自适应连续协调跟踪控制算法以提高系统的鲁棒性。通过Lyapunov稳定性理论证明了聚合跟踪误差的收敛性,所有USV的位置跟踪误差和速度跟踪误差有界并趋于一致,仿真验证了该算法的有效性。 展开更多
关键词 聚合跟踪误差 自适应连续控制 协调跟踪 分布式控制 边界层理论
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A PARAMETERIZED STUDY ON THE LOCAL SIMILARITY THEORY IN THE STABLE BOUNDARY LAYER MODEL
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作者 李兴生 唐承贤 许小金 《Science China Chemistry》 SCIE EI CAS 1991年第9期1131-1144,共14页
A 1-dimensional K-model parameterized by the local similarity theory is used to study the structure of the stably stratified boundary layer. The computed results are quite consistent with those of the second-order mom... A 1-dimensional K-model parameterized by the local similarity theory is used to study the structure of the stably stratified boundary layer. The computed results are quite consistent with those of the second-order moments model. Thus, the model can be used to improve the simulated results and the parameterized accuracy. 展开更多
关键词 STABLE boundary layer LOCAL SIMILARITY theory boundary layer model.
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On a Quasilinear Degenerate Parabolic Equation from Prandtl Boundary Layer Theory
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作者 OUYANG Miao 《Journal of Partial Differential Equations》 CSCD 2020年第2期119-142,共24页
The equation arising from Prandtl boundary layer theory (e)u/(e)t-(e)/(e)x1(a(u,x,t)(e)u/(e)xi)-fi(x)Diu+c(x,t)u=g(x,t)is considered.The existence of the entropy solution can be proved by BV estimate method.The intere... The equation arising from Prandtl boundary layer theory (e)u/(e)t-(e)/(e)x1(a(u,x,t)(e)u/(e)xi)-fi(x)Diu+c(x,t)u=g(x,t)is considered.The existence of the entropy solution can be proved by BV estimate method.The interesting problem is that,since a(·,x,t) may be degenerate on the boundary,the usual boundary value condition may be overdetermined.Accordingly,only dependent on a partial boundary value condition,the stability of solutions can be expected.This expectation is turned to reality by Kru(z)kov's bi-variables method,a reasonable partial boundary value condition matching up with the equation is found first time.Moreover,if axi(·,x,t)|x∈(e)Ω=a(·,x,t)|x∈(e)Ω=0 and fi(x)|x∈(e)Ω=0,the stability can be proved even without any boundary value condition. 展开更多
关键词 Prandtl boundary layer theory entropy solution Kru(z)kov's bi-variables method partial boundary value condition STABILITY
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AERMOD模式系统理论 被引量:62
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作者 杨多兴 杨木水 +3 位作者 赵晓宏 刘敏 邢可佳 仇蕾 《化学工业与工程》 CAS 2005年第2期130-135,共6页
作为新一代法规性质的稳态大气扩散模式,AERMOD将最新的大气边界层和大气扩散理论应用到空气污染扩散模式中。AERMOD具有下述特点:(1)按空气湍流结构和尺度的概念,湍流扩散由参数化方程给出,稳定度用连续参数表示;(2)中等浮力通量对流... 作为新一代法规性质的稳态大气扩散模式,AERMOD将最新的大气边界层和大气扩散理论应用到空气污染扩散模式中。AERMOD具有下述特点:(1)按空气湍流结构和尺度的概念,湍流扩散由参数化方程给出,稳定度用连续参数表示;(2)中等浮力通量对流条件采用非正态的PDF模式;(3)考虑了对流条件下浮力烟羽和混合层顶的相互作用;(4)AERMOD模式系统可以处理:地面源和高架源、平坦和复杂地形和城市边界层;(5)AERMAP提出了一个有效高度对流场的影响。示踪试验表明,AERMOD模拟的结果比较理想。 展开更多
关键词 AERMOD模式系统 大气边界层 大气扩散理论 有效高度
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各向异性复合材料圆柱薄壳轴压下的屈曲性能 被引量:4
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作者 王毅 罗永峰 沈惠申 《同济大学学报(自然科学版)》 EI CAS CSCD 北大核心 2002年第6期673-679,共7页
复合材料具有强度高 ,比强度大 ,材料性能可设计等优点 ,由各向异性复合材料制成的薄壳广泛地应用于海洋、航空和军工工业之中 .根据边界层理论 ,采用奇异摄动法 ,考虑非线性前屈曲、大挠度和初始几何缺陷的影响 ,分析在两端固支条件下 ... 复合材料具有强度高 ,比强度大 ,材料性能可设计等优点 ,由各向异性复合材料制成的薄壳广泛地应用于海洋、航空和军工工业之中 .根据边界层理论 ,采用奇异摄动法 ,考虑非线性前屈曲、大挠度和初始几何缺陷的影响 ,分析在两端固支条件下 ,各向异性层合圆柱壳在轴压下的屈曲和后屈曲性态 ,以挠度为摄动参数 ,求后屈曲平衡方程的渐进解并导出后屈曲平衡路径的四级表达式 ,同时给出了确定临界荷载的方法 . 展开更多
关键词 边界层理论 奇异摄动 屈曲荷载 后屈曲
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湍流激励下结构振动特性的半解析半数值算法研究 被引量:16
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作者 陈美霞 魏建辉 +1 位作者 乔志 李飘 《振动工程学报》 EI CSCD 北大核心 2011年第6期689-695,共7页
提出了一种基于随机激励理论计算结构在湍流激励下振动特性的半解析半数值算法。对经典的corcos模型给出的湍流脉动压力功率谱密度表达式进行离散得到湍流脉动压力功率谱密度矩阵作为输入,采用有限元边界元数值算法计算出考虑流固耦合... 提出了一种基于随机激励理论计算结构在湍流激励下振动特性的半解析半数值算法。对经典的corcos模型给出的湍流脉动压力功率谱密度表达式进行离散得到湍流脉动压力功率谱密度矩阵作为输入,采用有限元边界元数值算法计算出考虑流固耦合作用时结构的频响函数矩阵,进而结合随机理论计算出结构在湍流激励下速度响应的功率谱密度矩阵,同已有文献中解析法计算结果吻合较好,证明了计算方法的正确性。之后,将本文计算方法应用到湍流激励下单层圆柱壳振动特性的计算研究。结果表明:半解析半数值方法将经典的corcos模型和有限元边界元数值算法相结合,能够很好解决一些外形规则内部结构复杂的工程问题,具有较强的工程应用价值。 展开更多
关键词 随机激励理论 湍流边界层 半解析半数值法
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