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双三角翼的翼面压力分布与空间涡态相关分析 被引量:1
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作者 冯亚南 郑波 权少平 《空气动力学学报》 CSCD 北大核心 1999年第2期150-154,共5页
本文将双三角翼翼面测压试验结果与空间涡态观察测量结果进行了定性的相关对比分析,分析表明:垂直于双三角翼翼面的典型横截面上压力系数Cp展向分布与空间涡态有明显的对应关系,Cp分布的峰值数目反映了双三角翼的双涡态和单涡态... 本文将双三角翼翼面测压试验结果与空间涡态观察测量结果进行了定性的相关对比分析,分析表明:垂直于双三角翼翼面的典型横截面上压力系数Cp展向分布与空间涡态有明显的对应关系,Cp分布的峰值数目反映了双三角翼的双涡态和单涡态,Cp峰值随α变化反映了涡强随α的变化,Cp峰值所在展向位置反映着涡核的展向位置,Cp峰形的平坦反映了涡的破裂。 展开更多
关键词 大迎角 分离流 双三角翼 压力分布 空间涡
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大迎角跨音速三角翼漩涡特性及激波与涡干扰的数值模拟研究
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作者 李自启 梁斌 +1 位作者 罗松 刘敏 《教练机》 2016年第1期21-26,共6页
采用对流迎风分裂格式改进形式(AUSM+)和SST两方程湍流模型结合求解三维雷诺平均Navier Stokes(RANS)方程。通过对跨音速65°后掠尖前缘三角翼的数值模拟,研究了三角翼上翼面正激波的移动情况以及涡核破裂点变化情况。计算结果与实... 采用对流迎风分裂格式改进形式(AUSM+)和SST两方程湍流模型结合求解三维雷诺平均Navier Stokes(RANS)方程。通过对跨音速65°后掠尖前缘三角翼的数值模拟,研究了三角翼上翼面正激波的移动情况以及涡核破裂点变化情况。计算结果与实验对比表明:采用AUSM+格式和SST两方程湍流模型结合能够准确模拟出激波结构和大迎角下空间涡结构以及激波与涡相互干扰情况。 展开更多
关键词 迎风分裂格式 SST湍流模型 三角翼 激波 空间涡
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直驱式涡旋机接触力控制方法研究 被引量:1
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作者 方颢 蔡炯炯 +2 位作者 瞿晓 董桂丽 屠凯莉 《机电工程》 CAS 北大核心 2023年第10期1527-1534,共8页
针对涡旋机侧向密封过程中,动涡盘和静涡盘接触力难以控制的问题,结合动涡盘圆周平动特点,在分析了涡盘接触力模型的基础上,提出了一种基于法向-切向坐标系下的动涡盘运动控制策略以及主动柔顺控制方法。首先,介绍了经典柔顺控制的原理... 针对涡旋机侧向密封过程中,动涡盘和静涡盘接触力难以控制的问题,结合动涡盘圆周平动特点,在分析了涡盘接触力模型的基础上,提出了一种基于法向-切向坐标系下的动涡盘运动控制策略以及主动柔顺控制方法。首先,介绍了经典柔顺控制的原理,分析了XY直角坐标系下经典柔顺控制方法的不足;然后,提出了法向-切向坐标系这一概念,通过推导基于法向-切向坐标系下各运动变量之间的关系,对动涡盘的运动控制系统进行了总体设计;最后,采用MATLAB/Simulink软件搭建了涡旋机的接触力模型及其控制模型,并采用模型对上述方法进行了可行性验证,采用实验分别得到了动涡盘平动速率不变而接触力设定值改变时的实际接触力曲线,以及接触力设定值不变而动涡盘平动速率改变时的实际接触力曲线。研究结果表明:接触力的实际值与设定值的跟踪误差在2%以内;改变接触力的设定值后,接触力的实际值能在0.3 s左右跟踪到新的设定值;当动涡盘平动速率突然改变后,接触力的实际值能在0.2 s左右回到原来的平衡状态。以上结果说明,基于法向-切向坐标系下的主动柔顺控制方法可以有效地控制涡盘平动过程中的接触力。 展开更多
关键词 容积式压缩机 旋压缩机 盘工作空间 盘接触力模型 主动柔顺控制 坐标变换
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基于正交试验设计方法的短舱涡流片空间位置优选 被引量:2
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作者 肖旭东 雷武涛 +2 位作者 钱瑞战 许瑞飞 李星辉 《飞行力学》 CSCD 北大核心 2020年第5期27-31,69,共6页
以四台翼吊发动机运输机为研究对象,基于正交试验设计,通过N-S方程进行全机流场数值计算,研究了短舱涡流片的周向角、安装角和弦向位置对全机低速气动性能的影响,并优选出了最佳空间位置。研究结果表明:短舱涡流片诱导的空间涡能有效抑... 以四台翼吊发动机运输机为研究对象,基于正交试验设计,通过N-S方程进行全机流场数值计算,研究了短舱涡流片的周向角、安装角和弦向位置对全机低速气动性能的影响,并优选出了最佳空间位置。研究结果表明:短舱涡流片诱导的空间涡能有效抑制上翼面的流动分离,从而延缓失速,提升增升装置效率;短舱涡流片弦向位置对气动性能改善的贡献率最大,其次是安装角,周向角的贡献率最小;正交试验中最佳空间位置的短舱涡流片可使飞机最大升力系数提高4.53%,失速迎角增加2.8°。 展开更多
关键词 短舱流片 正交试验设计 N-S方程 低速气动性能 空间涡 增升装置
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基于PIV技术分析颗粒在湍流边界层中的行为 被引量:17
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作者 高天达 孙姣 +2 位作者 范赢 陈文义 轩瑞祥 《力学学报》 EI CSCD 北大核心 2019年第1期103-110,共8页
采用粒子图像测速技术(particle image velocimetry, PIV)在平板湍流边界层内开展实验研究,对比颗粒相及单相液体的平均速度剖面、湍流强度、雷诺应力等湍流统计量,分析颗粒在湍流边界层中的行为.利用空间多尺度局部平均涡量的概念提取... 采用粒子图像测速技术(particle image velocimetry, PIV)在平板湍流边界层内开展实验研究,对比颗粒相及单相液体的平均速度剖面、湍流强度、雷诺应力等湍流统计量,分析颗粒在湍流边界层中的行为.利用空间多尺度局部平均涡量的概念提取壁湍流发卡涡展向涡头(顺向涡)并统计其数量规律,得到不同法向位置处顺向涡周围流向脉动速度及流线的空间拓扑结构,比较分析顺向涡发展程度及周围的湍流相干结构.结果发现:与清水工况相比,颗粒相湍流边界层的缓冲层变薄、对数律区下移,湍流强度得到增强,雷诺应力在对数律区有所增大;颗粒的流向脉动速度在展向涡周围的分布与清水工况不同,颗粒能够被流体展向涡周围的猝发过程有效传递;颗粒相的顺向涡涡核较大,且随着法向位置的升高逐渐发展完整,涡和条带在流向上拉伸得更长;同时发现在两种工况下,顺向涡的左下方始终存在一个逆向涡,颗粒相逆向涡的形成弱于单相流体;两种工况下的顺向涡数量均随着法向位置的升高而减少,最后逐渐趋于稳定. 展开更多
关键词 两相流 粒子图像测速 湍流边界层 空间多尺度局部平均 顺向
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Vortex-Induced Vibration of Two Parallel Risers:Experimental Test and Numerical Simulation 被引量:1
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作者 HUANG Weiping ZHOU Yang CHEN Haiming 《Journal of Ocean University of China》 SCIE CAS 2016年第2期247-253,共7页
The vortex-induced vibration of two identical rigidly mounted risers in a parallel arrangement was studied using Ansys-CFX and model tests.The vortex shedding and force were recorded to determine the effect of spacing... The vortex-induced vibration of two identical rigidly mounted risers in a parallel arrangement was studied using Ansys-CFX and model tests.The vortex shedding and force were recorded to determine the effect of spacing on the two-degree-of-freedom oscillation of the risers.CFX was used to study the single riser and two parallel risers in 2–8D spacing considering the coupling effect.Because of the limited width of water channel,only three different riser spacings,2D,3D,and 4D,were tested to validate the characteristics of the two parallel risers by comparing to the numerical simulation.The results indicate that the lift force changes significantly with the increase in spacing,and in the case of 3D spacing,the lift force of the two parallel risers reaches the maximum.The vortex shedding of the risers in 3D spacing shows that a variable velocity field with the same frequency as the vortex shedding is generated in the overlapped area,thus equalizing the period of drag force to that of lift force.It can be concluded that the interaction between the two parallel risers is significant when the risers are brought to a small distance between them because the trajectory of riser changes from oval to curve 8 as the spacing is increased.The phase difference of lift force between the two risers is also different as the spacing changes. 展开更多
关键词 vortex-induced vibration RISER CFX drag force lift force
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Vortex Channel Modelling for the Radio Vortex System 被引量:1
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作者 Qibiao Zhu Tao Jiang 《China Communications》 SCIE CSCD 2018年第4期121-129,共9页
In this paper, a free-space vortex channel model of the radio vortex system is proposed to describe the propagation characteristics of vortex signals over the vortex channel. The key idea is to combine the Laguerre-Ga... In this paper, a free-space vortex channel model of the radio vortex system is proposed to describe the propagation characteristics of vortex signals over the vortex channel. The key idea is to combine the Laguerre-Gaussian(LG) modes in the optical field with the free-space propagation model in the radio field. The proposed free-space vortex channel model is derived from the electric field expression of the LG modes and the freespace channel transfer function of the freespace propagation model theoretically. Simulation results verify that the proposed model could reflect the vortex channel characteristics better than the currently used free-space propagation model. 展开更多
关键词 vortex channel model radiovortex FREE-SPACE laguerre-gaussian modes channel transfer function
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Design and implementation of space-time precoded systems with full diversity and lossless capacity
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作者 郑武 张海滨 +2 位作者 何晓炜 刘陈 宋文涛 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2008年第6期846-850,共5页
A new space-time(ST)code design is proposed based on the design criteria of space-time codes,which is applied to the MIMO systems with fewer receive antennas than transmit antennas.The space-time codes,referred to as ... A new space-time(ST)code design is proposed based on the design criteria of space-time codes,which is applied to the MIMO systems with fewer receive antennas than transmit antennas.The space-time codes,referred to as full diversity lossless capacity(FDLLC)ST code,achieve full transmit diversity and lossless equivalent channel capacity for ST precoded systems.Combined FDLLC-ST codes with channel codes,ST bit interleaved coded modulation(ST-BICM)system is constructed and an iterative detector/decoder is employed at the receiver.Simulations are presented.It is proved that the proposed design has good performance compared with other ST precoded MIMO systems. 展开更多
关键词 MIMO systems space-time codes turbo codes iterative decoder
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鳞鲀模式推进机理的数值研究 被引量:3
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作者 张睿谦 胡文蓉 《水动力学研究与进展(A辑)》 CSCD 北大核心 2020年第2期258-265,共8页
通过求解三维非定常不可压缩N-S方程对鳞鲀模式的游动进行了数值模拟,研究了鳞鲀模式游动的水动力学特性与流场特征,揭示鳞鲀模式游动的推进机理。结果表明,鳞鲀的背/臀鳍在一个波动周期内脱出两个非对称涡环,涡环中心诱导射流为鳞鲀提... 通过求解三维非定常不可压缩N-S方程对鳞鲀模式的游动进行了数值模拟,研究了鳞鲀模式游动的水动力学特性与流场特征,揭示鳞鲀模式游动的推进机理。结果表明,鳞鲀的背/臀鳍在一个波动周期内脱出两个非对称涡环,涡环中心诱导射流为鳞鲀提供推力;鳞鲀的推力分别依靠鳍面的波动和横侧摆动产生,背/臀鳍的安装角度使鳞鲀能更有效地利用这两部分的推力分量,且平衡沉浮力分量。鳞鲀所受推力随波动频率和幅度的增大而增大,随波长的增大先增大后减小,并且波长过大时,推进效率会急剧降低。相比于身体-尾鳍摆动(BCF)推进,鳞鲀模式具有极高的推进效率。与长鳍扭波推进模式相比,鳞鲀模式则具有更强的机动性。 展开更多
关键词 鳞鲀模式 空间涡结构 数值模拟
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超疏水壁面湍流边界层减阻机理的TRPIV实验 被引量:7
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作者 王二丹 田海平 +2 位作者 张静娴 姚朝辉 姜楠 《航空动力学报》 EI CAS CSCD 北大核心 2016年第12期2870-2877,共8页
利用高时间分辨率粒子图像测速(TRPIV)技术,开展超疏水壁面材料湍流边界层减阻机理的实验研究.在循环水槽中,对超疏水壁面和亲水壁面湍流边界层瞬时速度矢量场的时间序列进行了实验测量.得到了同一来流速度(0.17m/s)下超疏水壁面和亲水... 利用高时间分辨率粒子图像测速(TRPIV)技术,开展超疏水壁面材料湍流边界层减阻机理的实验研究.在循环水槽中,对超疏水壁面和亲水壁面湍流边界层瞬时速度矢量场的时间序列进行了实验测量.得到了同一来流速度(0.17m/s)下超疏水壁面和亲水壁面湍流边界层的平均速度、湍流度及雷诺切应力沿法向的分布规律.提出了空间多尺度局部平均涡量的概念,并以此为特征量检测壁湍流发卡涡展向涡头的中心位置.用条件采样及空间相位平均技术提取了不同法向位置发卡涡展向涡头周围流向脉动速度和流线的空间拓扑,对发卡涡展向涡头的俯仰角进行了对比,并从鞍点-焦点动力系统的角度分析了发卡涡展向涡头附近的流线拓扑特征.研究表明:雷诺数约为13 500时,相比亲水壁面,超疏水壁面实现了10.1%的减阻.超疏水壁面平均速度明显增大,雷诺切应力减小,流向湍流度减弱,发卡涡展向涡头俯仰角较小,近壁区相干结构的发展受到抑制. 展开更多
关键词 湍流减阻 超疏水壁面 湍流边界层 高时间分辨率粒子图像测速(TRPIV) 鞍点-焦点动力系统 空间多尺度局部平均
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Numerical studies towards practical large-eddy simulation 被引量:1
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作者 J.Boudet J.Caro +1 位作者 L.Shao E.Lév(?)que 《Journal of Thermal Science》 SCIE EI CAS CSCD 2007年第4期328-336,共9页
Large-eddy simulation developments and validations are presented for an improved simulation of turbulent internal flows. Numerical methods are proposed according to two competing criteria: numerical qualities (preci... Large-eddy simulation developments and validations are presented for an improved simulation of turbulent internal flows. Numerical methods are proposed according to two competing criteria: numerical qualities (precision and spectral characteristics), and adaptability to complex configurations. First, methods are tested on academic test-cases, in order to abridge with fundamental studies. Consistent results are obtained using adaptable finite volume method, with higher order advection fluxes, implicit grid filtering and "low-cost" shear-improved Smagorinsky model. This analysis particularly focuses on mean flow, fluctuations, two-point correlations and spectra. Moreover, it is shown that exponential averaging is a promising tool for LES implementation in complex geometry with deterministic unsteadiness. Finally, adaptability of the method is demonstrated by application to a configuration representative of blade-tip clearance flow in a turbomachine. 展开更多
关键词 LES adaptable methods VALIDATION
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Large eddy simulation of a 3-D spatially developing turbulent round jet 被引量:2
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作者 ZHANG HuiQiang RONG Yi +1 位作者 WANG Bing WANG XiLin 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第11期2916-2923,共8页
A three-dimensional large eddy simulation (LES) of a spatially developing round jet is carried out in cylindrical coordinates using a dynamic subgrid model with strong inflow instability. Evolutions of large-scale v... A three-dimensional large eddy simulation (LES) of a spatially developing round jet is carried out in cylindrical coordinates using a dynamic subgrid model with strong inflow instability. Evolutions of large-scale vortex structures represented by tangential vortices are obtained and compared with flow visualization. Also presented are three-dimensional spatial evolutions of coherent structure, which are of quasi two-dimensional Kelvin-Helmholtz instability and vortex rings as well as breaking up of the vortex rings with fully three-dimensional characteristics. Predicted results of mean velocity and turbulent intensity agree well with experiments. They are also compared with the results predicted by LES using standard Smagorinsky model and show good self-similarity. Turbulence spectrum of the predicted velocity shows the -5/3 decay for higher wave number, as expected for turbulent round jet flows. In addition, fl-test and y-test are carded out for the instantaneous velocity, showing that the present LES method can successfully predict the hierarchical structure of round jet. 展开更多
关键词 large eddy simulation round jet spatially developing flow large-scale structure hierarchical structure
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Dynamic mode decomposition of hairpin vortices generated by a hemisphere protuberance 被引量:8
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作者 TANG ZhanQi JIANG Nan 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2012年第1期118-124,共7页
We present dynamic mode decomposition (DMD) for studying the hairpin vortices generated by hemisphere protuberance measured by two-dimensional (2D) time-resolved (TR) particle image velocimetry (PIV) in a water channe... We present dynamic mode decomposition (DMD) for studying the hairpin vortices generated by hemisphere protuberance measured by two-dimensional (2D) time-resolved (TR) particle image velocimetry (PIV) in a water channel. The hairpins dynamic information is extracted by identifying their dominant frequencies and associated spatial structures. For this quasi-periodic data system, the resulting main Dynamic modes illustrate the different spatial structures associated with the wake vortex region and the near-wall region. By comparisons with proper orthogonal decomposition (POD), it can be concluded that the dynamic mode concentrates on a certain frequency component more effectively than the mode determined by POD. During the analysis, DMD has proven itself a robust and reliable algorithm to extract spatial-temporal coherent structures. 展开更多
关键词 hairpin vortices hemisphere protuberance time-resolved particle image velocimetry dynamic mode decomposition proper orthogonal decomposition
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Vortex and Gaussian Solitons of (3+1)-Dimensional Spatially Modulated Cubic-Quintic-Septimal Nonlinear Schrdinger Equation with External Potential
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作者 徐云杰 《Communications in Theoretical Physics》 SCIE CAS CSCD 2017年第10期478-482,共5页
Based on the variable separation principle and the similarity transformation, vortex soliton solution of a (3+1)-dimensional cubie-quintic-septimal nonlinear Schrodinger equation with spatially modulated nonlineari... Based on the variable separation principle and the similarity transformation, vortex soliton solution of a (3+1)-dimensional cubie-quintic-septimal nonlinear Schrodinger equation with spatially modulated nonlinearity under the external potential are obtained in the spatially modulated cubic-quintic-septimal nonlinear media. If the topological charge m = 0 and m ≠0, Gaussian solitons and vortex solitons can be constructed respectively. The shapes of vortex soliton possess similar structures when the value of l - m is same. Moreover, all phases of vortex solitons exist m-jump with the change of every jump as 2π/m-jumps, and thus totally realize the azimuthal change of 21r around their cores. 展开更多
关键词 (3+1)-dimensional cubic-quintic-septimal nonlinear media sPatially modulated nonlinearity vor-tex solitons Gaussian solitons
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Numerical Investigation of Flutter Stability in Subsonic Space Turbine Blisk with Emphasis on Cut-on/Cut-off Modes and Interblade Phase Angles 被引量:1
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作者 Hakim Ferria Pascal Ferrand +1 位作者 Franois Pacull Stéphane Aubert 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第6期492-499,共8页
The so-called blisks,i.e.integrally bladed disks,are characterized by very low viscous material damping and make the flutter prediction much more critical.In that framework,a two-dimensional numerical study of a space... The so-called blisks,i.e.integrally bladed disks,are characterized by very low viscous material damping and make the flutter prediction much more critical.In that framework,a two-dimensional numerical study of a space turbine blisk featuring complex deformation of blades and high eigenfrequency(>40kHz)is performed.The simulations are based on unsteady Reynolds Averaged Navier Stokes computations linearized in the frequency domain and consist in the superposition of an unsteady linear(in time)pressure field,generated by a harmonic perturbation,upon a steady nonlinear(in space)flow.The aerodynamic damping coefficient is calculated over a range of nodal diameters,and the blades are predicted aeroelastically stable.However,violent changes occur and are rather critical since sudden and large deviations in stability appear.In that context,the nature of the waves propagating from the cascade are evaluated.Such an approach provides fundamental knowledge about the perturbations which can either propagate to the far-field(cut-on mode)or decay(cut-off mode).It is expected that the ability of the flow to damp or to amplify the blade motion is strongly affected by the way unsteady perturbations are transferred from the cascade to the far-field.The nature of the waves are first assessed from the aforementioned linearized results,then they are evaluated analytically and finally compared.A good agreement is found despite the strong assumptions of the analytical model.The results show a clear correlation between the cut-on/cut-off conditions and stability.The least stable configuration corresponds to cut-off mode at the inlet and no wave at the outlet.Without outgoing waves from the cascade,the blade is prone to be less stable:the energy from the blades vibration is necessarily dissipated or sent out by the cascade. 展开更多
关键词 subsonic flutter LRANS BLISK cut-on/cut-off mode interblade phase angle nodal diameter.
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Recent understanding on the subgrid-scale modeling of large-eddy simulation in physical space 被引量:4
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作者 FANG Le SHAO Liang BERTOGLIO J.-P. 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS 2014年第12期2188-2193,共6页
In the last 50 years,the methodology of large-eddy simulation(LES)has been greatly developed,while lots of different subgridscale(SGS)models have appeared.However,the understanding of the procedure of SGS modeling is ... In the last 50 years,the methodology of large-eddy simulation(LES)has been greatly developed,while lots of different subgridscale(SGS)models have appeared.However,the understanding of the procedure of SGS modeling is still not clear.The present contribution aims at reviewing the recent SGS models and,more importantly,expressing our recent understanding on the SGS modeling of LES in physical space.Taking the Kolmogorov equation for filtered quantities(KEF)as an example,it is argued that the KEF alone is not enough to be a closure method.Three physical laws are then introduced to complete this closure procedure and are expected to inspire the future researches of SGS modeling. 展开更多
关键词 large-eddy simulation subgrid-scale modeling Koimogorov equation
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A Comparative Study of the Local Heat Transfer Distributions Around Various Surface Mounted Obstacles
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作者 Robert Wyssmann Dirk Ullmer +1 位作者 Alexandros Terzis Peter Ott 《Journal of Thermal Science》 SCIE EI CAS CSCD 2014年第2期169-176,共8页
In many engineering applications,heat transfer enhancement techniques are of vital importance in order to ensure reliable thermal designs of convective heat transfer applications.This study examines experimentally the... In many engineering applications,heat transfer enhancement techniques are of vital importance in order to ensure reliable thermal designs of convective heat transfer applications.This study examines experimentally the heat transfer characteristics on the base plate around various surface mounted obstacles.Local convection coefficients are evaluated in the vicinity of each individual protruding body with great spatial resolution using the transient liquid crystal technique.Five different obstacles of constant height-to-hydraulic diameter ratio(~1.3) are considered.These include:a cylinder,a square,a triangle,a diamond and a vortex generator of delta wing shape design.The experiments were carried out over a range of freestream Reynolds numbers,based on the hydraulic diameter of each obstacle,varying from 4,000 to 13,000.The results indicate a negligible effect of the flow speed on the heat transfer topological structure and a considerable effect of the obstacle geometry on the level and distribution of heat transfer enhancement. 展开更多
关键词 surface obstacles heat transfer enhancement transient liquid crystal technique
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