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用分析温度场的程序计算定常无旋流动
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作者 郑作昌 《力学与实践》 CSCD 北大核心 1995年第2期57-59,共3页
用分析温度场的程序计算定常无旋流动郑作昌(北京大学力学系,北京100871)目前流行的用于热传导分析的计算机程序很多,如ADINAT,SAP5-T等.但它们的能力却远远超出了分析热传导问题。本文通过分析热传导问题与其... 用分析温度场的程序计算定常无旋流动郑作昌(北京大学力学系,北京100871)目前流行的用于热传导分析的计算机程序很多,如ADINAT,SAP5-T等.但它们的能力却远远超出了分析热传导问题。本文通过分析热传导问题与其它一些连续场问题在数学上的等价性,... 展开更多
关键词 流体力学 温度场 定常无旋流动
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物面上流函数的值必须由流动条件来确定
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作者 冯振宇 《中国大学教学》 1993年第5期43-44,共2页
关键词 物面 流函数 流动条件 切线方向 表面轮廓 轮廓线 平行直线 任意选取 无旋流动 外廓线
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几种物理场的相似性及其在有限元分析中的实现
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作者 龙军 孙新岭 《后勤工程学院学报》 2003年第1期61-64,共4页
用数学方法对渗流、杆的扭转、流体的无粘性不可压缩无旋流动、电传导中的电压场等几种物理场方程进行推导得到各自的控制方程,通过比较分析这几种物理场与温度场控制方程的异同,得出了温度场的计算机辅助有限元分析软件也可用于分析... 用数学方法对渗流、杆的扭转、流体的无粘性不可压缩无旋流动、电传导中的电压场等几种物理场方程进行推导得到各自的控制方程,通过比较分析这几种物理场与温度场控制方程的异同,得出了温度场的计算机辅助有限元分析软件也可用于分析计算这类物理场的结论。为分析解决此类问题提供了一种新的思路。 展开更多
关键词 有限元分析 渗流 杆扭转 无粘性不可压缩无旋流动 电压场 控制方程 物理场 温度场
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带尾涡面的三维复杂外形亚音速有限元计算
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作者 夏南 庄礼贤 张宏 《南昌工程学院学报》 CAS 1994年第S1期30-35,共6页
一、前言 对三维复杂外形的亚音速有限元分析系采用全速势方程作控制方程,用Galerkin加权余量法形成有限元方程。采用四面体线性插值单元分别对不可压流与马赫数1以下的可压流进行了计算,并给出在不同攻角下各剖面的速度、压力分布及气... 一、前言 对三维复杂外形的亚音速有限元分析系采用全速势方程作控制方程,用Galerkin加权余量法形成有限元方程。采用四面体线性插值单元分别对不可压流与马赫数1以下的可压流进行了计算,并给出在不同攻角下各剖面的速度、压力分布及气动力系数。 展开更多
关键词 全速势方程 涡面 气动力系数 线性插值 加权余量法 无旋流动 带尾 压力分布 子午面 四面体单元
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悉尼燃烧器钝体回流区的大涡模拟
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作者 唐鹏 耿雪 +2 位作者 张济民 董佳宾 方曙东 《池州学院学报》 2014年第6期41-43,共3页
通过大涡模拟方法(LES),对悉尼旋流燃烧器冷态流场下的无旋算例进行了计算,研究了不同雷诺数下钝体回流区的流场特性。大涡模拟结果和实验值符合的较好。数值计算表明,LES方法可以较好的计算冷态流场,钝体回流区的长度随着雷诺数变化不... 通过大涡模拟方法(LES),对悉尼旋流燃烧器冷态流场下的无旋算例进行了计算,研究了不同雷诺数下钝体回流区的流场特性。大涡模拟结果和实验值符合的较好。数值计算表明,LES方法可以较好的计算冷态流场,钝体回流区的长度随着雷诺数变化不明显,在雷诺数增大时钝体回流区的逆压梯度增大,流场颈部收缩现象更加明显。 展开更多
关键词 悉尼燃烧器 无旋流动 大涡模拟 钝体回流区
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Oceanic internal solitary waves in three-layer fluids of great depth 被引量:1
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作者 Zi'an Wang Zhan Wang Chunxin Yuan 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第2期46-59,I0002,共15页
This paper is mainly concerned with modeling nonlinear internal waves in the ocean of great depth.The ocean is assumed to be composed of three homogeneous fluid layers of different densities in a stable stratified con... This paper is mainly concerned with modeling nonlinear internal waves in the ocean of great depth.The ocean is assumed to be composed of three homogeneous fluid layers of different densities in a stable stratified configuration.Based on the Ablowitz-Fokas-Musslimani formulation for irrotational flows,strongly nonlinear and weakly nonlinear models are developed for the“shallow-shallow-deep”and“deep-shallow-deep”scenarios.Internal solitary waves are computed using numerical iteration schemes,and their global bifurcation diagrams are obtained by a numerical continuation method and compared for different models.For the“shallow-shallow-deep”case,both mode-1 and mode-2 internal solitary waves can be found,and a pulse broad-ening phenomenon resulting in conjugate flows is observed in the mode-2 branch.While in the“deep-shallow-deep”situation,only mode-2 solitary waves can be obtained.The existence and stability of mode-2 internal solitary waves are confirmed by solving the primitive equations based on the MITgcm model. 展开更多
关键词 Internal wave Interfacial wave Solitary wave
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Flow Development through HP&LP Turbines,PartⅠ:Inward Rotating Cavity Flow with Superimposed Throughflow
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作者 GAO Jinhai DU Qiang +4 位作者 LIU Jun LIU Guang WANG Pei LIU Hongrui DU Meimei 《Journal of Thermal Science》 SCIE EI CAS CSCD 2017年第4期297-307,共11页
With the aid of numerical method, both flow field and its accompanied loss mechanism within the rotating cavity are investigated in detail in the 1^(st) part of the two parts paper. For ease of comparison, rotating ca... With the aid of numerical method, both flow field and its accompanied loss mechanism within the rotating cavity are investigated in detail in the 1^(st) part of the two parts paper. For ease of comparison, rotating cavity is further classified as the rotor-stator cavity case and the rotor-rotor cavity case. Results indicate that flow within both kinds of the cavity act as the inviscid flow except that the flow near walls, neighboring the lower G region and in the vicinity of the rotating orifices. In the regions except such inviscid-flow-dominate domains, the theoretical core rotation factor can be safely used to predict the swirl ratio within the cavity. When detailed flow pattern is considered, Ekman-type flow exists near periphery of the surface's boundary layer where viscous effect is non-negligible. However, due to the complex profile of the simulated cavity case, vortices structure is varied within the cavity. By comparison, swirl ratio can be used to predict the magnitude of loss. Due to the relatively evident rotating effects of the rotor-rotor cavity, swirl ratio even increases to 1.4 in the current model, which means that flow is moving faster than the surrounding disc. Further investigation finds that this kind of highly rotating flow is accompanied with serious undesirable pressure loss. Parenthetically, unlike its counterpart, swirl ratio above 1.0 doesn't happen when fluid passes through the rotor-stator cavity. So it is suggested that rotor-rotor flow cavity with the superimposed inward throughflow should be avoided in the engine design or certain measurements should be provided when such structure design is unavoidable. Simulation done in the current paper is meaningful since these dimensional parameters are typical in the design of state-of-art. Relatively lower range of Re_φ and C_w is not considered in the current two parts paper. 展开更多
关键词 Turbines Inward rotating cavity flow Superimposed throughflow Flow pattern
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