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Shape-induced phase transition of vortex domain structures in ferroelectric nanodots and their controllability by electrical and mechanical loads 被引量:1
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作者 Jianyi Liu Weijin Chen Yue Zheng 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2017年第2期81-87,共7页
Shape-induced phase transition of vortex domain structures (VDSs) in BaTiO3 (BT) nanodots under open circuit boundary condition have been investigated using an effective Hamiltonian method. Our calculation indicat... Shape-induced phase transition of vortex domain structures (VDSs) in BaTiO3 (BT) nanodots under open circuit boundary condition have been investigated using an effective Hamiltonian method. Our calculation indicates the tetragonal VDS missing in cubic BT nanodots can be induced by varying the shape of a nanodot from cube to platelet. Interestingly, a novel VDS is found in BT nanoplatelets in our simulations. Further investigation shows that it is a result of compromise between the ground state and the symmetry of the shape of the nanodot. Furthermore, based on the novel VDS, routes of controlling VDSs governed by homogeneous electric field and uniform stress are discussed. In particular, our results show the possibility of designing multi-states devices based on a single VDS. ~ 2017 The Authors. Published by Elsevier Ltd on behalf of The Chinese Society of Theoretical and Applied Mechanics. 展开更多
关键词 vortex domain structure Ferroelectric phase transition shape Symmetry Nanodots
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Study on the Wake Shape behind a Wing in Ground Effect Using an Unsteady Discrete Vortex Panel Method
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作者 Cheolheui Han Spyros A. Kinnas 《Open Journal of Fluid Dynamics》 2013年第4期261-265,共5页
The unsteady evolution of trailing vortex sheets behind a wing in ground effect is simulated using an unsteady discrete vortex panel method. The ground effect is included by image method. The present method is validat... The unsteady evolution of trailing vortex sheets behind a wing in ground effect is simulated using an unsteady discrete vortex panel method. The ground effect is included by image method. The present method is validated by comparing the simulated wake roll-up shapes to published numerical results. When a wing is flying in a very close proximity to the ground, the optimal wing loading is parabolic rather than elliptic. Thus, a theoretical model of wing load distributions is suggested, and unsteady vortex evolutions behind lifting lines with both elliptic and parabolic load distributions are simulated for several ground heights. For a lifting line with elliptic and parabolic loading, the ground has the effect of moving the wingtip vortices laterally outward and suppressing the development of the vortex. When the wing is in a very close proximity to the ground, the types of wing load distributions does not affect much on the overall wake shapes, but parabolic load distributions make the wingtip vortices move more laterally outward than the elliptic load distributions. 展开更多
关键词 WAKE shape WING in Ground Effect UNSTEADY DISCRETE vortex Method
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Dynamic performance and wake structure of flapping plates with different shapes 被引量:3
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作者 Gao-Jin Li Nan-Sheng Liu Xi-Yun Lu 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2014年第6期800-808,共9页
The dynamic performance and wake structure of flapping plates with different shapes were studied using multi-block lattice Boltzman and immersed boundary method.Two typical regimes relevant to thrust behavior are iden... The dynamic performance and wake structure of flapping plates with different shapes were studied using multi-block lattice Boltzman and immersed boundary method.Two typical regimes relevant to thrust behavior are identified.One is nonlinear relation between the thrust and the area moment of plate for lower area moment region and the other is linear relation for larger area moment region.The tendency of the power variation with the area moment is reasonably similar to the thrust behavior and the efficiency decreases gradually as the area moment increases.As the mechanism of the dynamic properties is associated with the evolution of vortical structures around the plate,the formation and evolution of vortical structures are investigated and the effects of the plate shape,plate area,Strouhal number and Reynolds number on the vortical structures are analyzed.The results obtained in this study provide physical insight into the understanding of the mechanisms relevant to flapping locomotion. 展开更多
关键词 Dynamics of flapping plate Flapping locomotion Plate shape vortex dynamics
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Tight focusing of axially symmetric polarized vortex beams 被引量:2
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作者 周哲海 郭阳宽 祝连庆 《Chinese Physics B》 SCIE EI CAS CSCD 2014年第4期251-255,共5页
Tight focusing of axially symmetric polarized vortex beams is studied numerically based on vector diffraction theory. The mathematical expressions for the focused fields are derived. Simulation results show that the f... Tight focusing of axially symmetric polarized vortex beams is studied numerically based on vector diffraction theory. The mathematical expressions for the focused fields are derived. Simulation results show that the focused fields and phase distributions at focus are largely influenced by both the polarization order and topological charge of the incident beams. Moreover, focal spots with flat-topped or tightly-focused patterns can be flexibly achieved by carefully choosing the polar- ization order and the topological charge, which confirms the potential of such beams in wide applications, such as optical tweezers, laser printing, lithography, and material processing. 展开更多
关键词 axially symmetric polarization vortex beams tight focusing beam shaping
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Effect of air core on the shape and discharge of the outflow through a bottom outlet
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作者 Yiyi Ma Yu Qian David Z. Zhu 《Theoretical & Applied Mechanics Letters》 CAS 2013年第2期72-76,共5页
Experiments were conducted to study the generation of air core and its effect on the outflow shape and discharge in a cylindrical water tank with a bottom well-designed outlet. Depending on the stages of the air core ... Experiments were conducted to study the generation of air core and its effect on the outflow shape and discharge in a cylindrical water tank with a bottom well-designed outlet. Depending on the stages of the air core in the tank, the outflow shape can vary from a smooth water jet to a smooth spindle shape with air-core, and to water sprays. The diameter of the nozzle size also has influence on the outflow pattern. The existence of the penetrated air core can dramatically reduce the outflow discharge, with the discharge coefficient decreasing with the nozzle diameter. 展开更多
关键词 air core DISCHARGE outflow shape SPRAY vortex
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A saw-tooth plasma actuator for film cooling efficiency enhancement of a shaped hole
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作者 李国占 俞建阳 +2 位作者 刘华坪 陈浮 宋彦萍 《Plasma Science and Technology》 SCIE EI CAS CSCD 2017年第8期125-137,共13页
This paper reports the large eddy simulations of the effects of a saw-tooth plasma actuator and the laidback fan-shaped hole on the film cooling flow characteristics, and the numerical results are compared with a corr... This paper reports the large eddy simulations of the effects of a saw-tooth plasma actuator and the laidback fan-shaped hole on the film cooling flow characteristics, and the numerical results are compared with a corresponding standard configuration(cylindrical hole without the sawtooth plasma actuator). For this numerical research, the saw-tooth plasma actuator is installed just downstream of the cooling hole and a phenomenological plasma model is employed to provide the 3D plasma force vectors. The results show that thanks to the downward force and the momentum injection effect of the saw-tooth plasma actuator, the cold jet comes closer to the wall surface and extends further downstream. The saw-tooth plasma actuator also induces a new pair of vortex which weakens the strength of the counter-rotating vortex pair(CRVP) and entrains the coolant towards the wall, and thus the diffusion of the cold jet in the crossflow is suppressed.Furthermore, the laidback fan-shaped hole reduces the vertical jet velocity causing the disappearance of downstream spiral separation node vortices, this compensates for the deficiency of the saw-tooth plasma actuator. Both effects of the laidback fan-shaped hole and the saw-tooth plasma actuator effectively control the development of the CRVP whose size and strength are smaller than those of the anti-counter rotating vortex pair in the far field, thus the centerline and the spanwise-averaged film cooling efficiency are enhanced. The average film cooling efficiency is the biggest in the Fan-Dc=1 case, which is 80% bigger than that in the Fan-Dc=0 case and 288% bigger than that in the Cyl-Dc=0 case. 展开更多
关键词 actuator shaped downstream tooth averaged rotating vortex installed turbulent momentum
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Flow around three rectangular cylinders arranged in connected and separated Y-shape
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作者 Zhifu Gu Yan Li 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2005年第4期336-341,共6页
Characteristics of cross flow around three rectangular cylinders with two aspect ratios of breadth to width arranged in connected and separated Y-shape at various angles of incident flow were studied by means of force... Characteristics of cross flow around three rectangular cylinders with two aspect ratios of breadth to width arranged in connected and separated Y-shape at various angles of incident flow were studied by means of force measurement in a wind tunnel. Flow visualizations with smoke-wire technique for typical cases were also given. Different types of flow patterns were formed for individual models at different angles of incident flow. From the results of fluctuating velocity measurement in the wake, features of vibration were determined. It shows that as the wind blows along the lines of one limb or rectangular cylinder of the model, oscillation is weak, whereas when the wind blows along the bisector lines of two limbs or cylinders, strong vibration is observed. It is associated with the regular vortex shedding. 展开更多
关键词 Rectangular cylinders. vortex-induced vibration Flow visualization Y-shape
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Analysis of VIV for Barrel-Shaped Mast with Covering Ice by HPD-S Method
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作者 张营川 马骏 赵德有 《China Ocean Engineering》 SCIE EI 2009年第4期763-768,共6页
The vortex-induced vibrations (VIV) of barrel-shaped mast are calculated by three numerical metods, i.e. New- mark- β, HPD-L (High Precision Direct integration scheme-Linear form), and HPD-S (High Precision Dire... The vortex-induced vibrations (VIV) of barrel-shaped mast are calculated by three numerical metods, i.e. New- mark- β, HPD-L (High Precision Direct integration scheme-Linear form), and HPD-S (High Precision Direct integration scheme-Sinusoidal form). According to the measured value, the accuracy curves are given to show the advantages of HPD-S method over others. Based on the comparison above, HPD-S method is used to calculate the influence of ice covering on the mast to VIV responses. It has been proved that the vortex-induced responses of barrel-shaped mast are changed along with ice thicknesses and types. 展开更多
关键词 vortex-Indued Vibration VIV) barrel-shaped mast covering ice precise integration method
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基于SVS算法优选整形正则化参数的WLSSI谱反演方法研究 被引量:1
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作者 乐友喜 付俊楠 葛传友 《石油地球物理勘探》 北大核心 2025年第2期440-451,共12页
谱反演方法是研究非平稳地震信号的有效手段,在地震信号处理、分析和综合解释领域发挥了重要的作用。文中提出一种基于分群涡流搜索(SVS)算法优选整形正则化参数的加权最小二乘谱反演(WLSSISVSOSR)方法。该方法从一般正问题的理论公式出... 谱反演方法是研究非平稳地震信号的有效手段,在地震信号处理、分析和综合解释领域发挥了重要的作用。文中提出一种基于分群涡流搜索(SVS)算法优选整形正则化参数的加权最小二乘谱反演(WLSSISVSOSR)方法。该方法从一般正问题的理论公式出发,反演得到地震信号的傅里叶级数系数,然后将整形正则化思想引入加权最小二乘谱反演中,基于谱反演方法构造了一种整形正则化算子;采用分群涡流搜索算法对整形正则化参数进行优选,较好地克服了反演过程中的收敛速度慢和稳定性差的问题,获得了地震信号较为稳定的时―频域分布特征。模型测试及实际资料处理结果表明:该方法具有很好的时频域分辨率及能量聚焦性,能够识别含油气储层的优势频率范围;利用优势频率的瞬时振幅特征,可以基本确定含油气储层的横向分布范围,从而实现对含油气储层的精细刻画和描述。 展开更多
关键词 谱反演 整形正则化 分群涡流搜索算法 加权最小二乘 时频谱
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淤积体对排沙漏斗水沙分离性能的影响机理研究 被引量:2
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作者 李琳 顾怀猛 谭义海 《水利学报》 北大核心 2025年第2期227-239,共13页
为揭示淤积体对排沙漏斗水沙分离性能的影响机理,开展不同厚度淤积体下的浑水模型试验,并利用声学多普勒流速仪量测三维流场,观测空气涡形态变化。研究结果表明:不同进流量下排沙耗水率均随淤积体厚度的增大而增大,泥沙截除率随淤积体... 为揭示淤积体对排沙漏斗水沙分离性能的影响机理,开展不同厚度淤积体下的浑水模型试验,并利用声学多普勒流速仪量测三维流场,观测空气涡形态变化。研究结果表明:不同进流量下排沙耗水率均随淤积体厚度的增大而增大,泥沙截除率随淤积体厚度增加而逐渐降低,不同淤积厚度下排沙耗水率是无淤积体时的1.27~2.14倍,泥沙截除率降幅33%~57%;淤积体导致漏斗流场特性发生改变,泥沙淤积厚度增加使空气涡由无淤积时的稳定贯穿变化至频繁摆动并偏离排沙底孔,不同水沙条件下涡径减小5.95%~53.07%,使排沙耗水率增大;漏斗室内自由涡范围和强度随淤积体厚度增加而减小,设计流量下切向流速平均减小20%~55%,位于强迫涡和自由涡间的环形低流速带宽度与无淤积情况相比增大33%~40%,不利于水沙的螺旋流分离,横向环流强度减弱,不利于泥沙向底孔输移,致使淤积加剧,从而进一步削减旋流强度;径向及垂向紊动强度随泥沙淤积厚度增加分别增大10%~110%和12%~120%,致使悬移质泥沙难以沉降,截除率大幅降低。 展开更多
关键词 排沙漏斗 模型试验 淤积体 空气涡形态 流场特性
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海豹胡须柱杆件周围流场与气动噪声特性
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作者 朱剑月 王亚正 +1 位作者 徐俊起 庞加斌 《同济大学学报(自然科学版)》 北大核心 2025年第4期652-660,共9页
基于海豹胡须能有效抑制涡激振动的特殊结构,数值分析了海豹胡须柱杆件周围流场与气动噪声特性。在声学风洞中进行了气动噪声测试,并与具有相同特征长度的圆柱以及椭圆柱杆件进行对比。结果表明,海豹胡须柱鞍面与节点面交错排列的几何... 基于海豹胡须能有效抑制涡激振动的特殊结构,数值分析了海豹胡须柱杆件周围流场与气动噪声特性。在声学风洞中进行了气动噪声测试,并与具有相同特征长度的圆柱以及椭圆柱杆件进行对比。结果表明,海豹胡须柱鞍面与节点面交错排列的几何结构引发流体三维分离,剪切层之间的相互作用减弱,导致尾迹中没有明显的拟序结构、尾迹稳定性显著提升、几何体表面升力脉动被抑制;海豹胡须柱破坏了圆柱尾流规律性脱落的卡门涡街,抑制了所产生气动噪声的谐频峰值,多数频段内声压级幅值降低。气动噪声风洞测试结果验证了数值模拟的准确性。 展开更多
关键词 海豹胡须柱 气动噪声 流场特性 涡脱落 谱本征正交分解
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侧壁多孔射流压比对稳态总压畸变模拟的影响规律
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作者 张冬晨 项效镕 +3 位作者 刘翼腾 任三群 赵巍 赵庆军 《推进技术》 北大核心 2025年第5期265-277,共13页
针对发动机地面与高空模拟试验中不同形式总压畸变在线模拟的需求,采用数值仿真方法,研究了侧壁多孔射流畸变模拟器不同射流压比下肾形反旋涡对的沿程演变规律,以及其对总压畸变分布与畸变指数的影响机制。同时,提出了一种总压畸变图谱... 针对发动机地面与高空模拟试验中不同形式总压畸变在线模拟的需求,采用数值仿真方法,研究了侧壁多孔射流畸变模拟器不同射流压比下肾形反旋涡对的沿程演变规律,以及其对总压畸变分布与畸变指数的影响机制。同时,提出了一种总压畸变图谱特征参数牵引下的畸变模拟器侧壁单孔/双孔射流周向组合排布与压比调控方法,在总压恢复系数基本维持不变的情况下总压畸变指数模拟相对偏差可控制在5%以内。研究结果表明,侧壁单孔射流所致肾形反旋涡对与射流柱的沿程掺混直接影响总压损失分布特征,低压区穿透深度、尺寸大小均随射流压比增大而增加但增速趋缓;双孔射流夹角与射流压比单调影响两组反旋涡对的3种形态,低压区穿透深度、尺寸大小均随射流压比增大而增加,但随射流夹角的变化同反旋涡对的3种形态密切相关;单孔与双孔射流下总压畸变指数随射流压比先增后减,且随着射流夹角增加畸变指数变化拐点所对应的射流压比逐步增大。 展开更多
关键词 畸变模拟 稳态畸变 射流 肾形涡结构 总压分布 畸变指数
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近壁流向涡对多排孔气膜冷却效率影响的实验研究
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作者 王佳男 崔晓峰 +1 位作者 林翅翔 戴韧 《动力工程学报》 北大核心 2025年第5期654-661,共8页
在平板气膜实验台上安装涡流发生器生成流向涡,研究了叶栅端区二次流对多排扇形孔气膜冷却效率的影响。实验测量了四排气膜孔的绝热气膜冷却效率,并基于Sellers公式分析各排孔气膜冷却效率受影响程度的差异。结果表明:受涡旋向的影响,... 在平板气膜实验台上安装涡流发生器生成流向涡,研究了叶栅端区二次流对多排扇形孔气膜冷却效率的影响。实验测量了四排气膜孔的绝热气膜冷却效率,并基于Sellers公式分析各排孔气膜冷却效率受影响程度的差异。结果表明:受涡旋向的影响,气膜覆盖沿涡的运动路线发生扭曲,气膜冷却效率下降,在第二排涡流核心处形成热斑;涡流的影响程度与气膜吹风比有关,近壁涡主要降低了前两排孔的气膜冷却效率;第一排孔的气膜冷却效率下降明显,而第二排孔的降幅减少,对后排孔的影响逐排减弱,第三排孔以后的气膜基本不受影响。 展开更多
关键词 流向涡 扇形孔 气膜冷却效率 气膜叠加效应
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考虑机身前体影响的S弯进气道大迎角性能试验
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作者 全景阁 韩珊珊 +2 位作者 冯晓强 郁新华 孙琰 《火箭推进》 北大核心 2025年第2期52-61,共10页
考虑融合体机身前体的影响,对一种高机动隐身无人机背负式S弯进气道开展了大迎角状态下的气动性能试验研究。综合考虑流量系数、马赫数、迎角和侧滑角的影响,获得了进气道在亚、跨音速范围内的气动特性,重点关注融合体机身前体对S弯进... 考虑融合体机身前体的影响,对一种高机动隐身无人机背负式S弯进气道开展了大迎角状态下的气动性能试验研究。综合考虑流量系数、马赫数、迎角和侧滑角的影响,获得了进气道在亚、跨音速范围内的气动特性,重点关注融合体机身前体对S弯进气道大迎角性能的影响。结果表明:考虑机身前体影响后,机身前体分离涡对进气道产生有利影响,S弯进气道大迎角气动性能得到改善,表现出和常规背负式S弯进气道不同的变化趋势;随着迎角增加,进气道大迎角总压恢复系数不再减小,而是在某一临界迎角后开始增加,畸变指数不再增加,而是在临界迎角后开始降低,进气道大迎角性能不再变差,而是保持较好的性能;侧滑角对进气道性能的不利影响减弱,小侧滑大迎角状态下进气道依然可以保持较高的性能。 展开更多
关键词 融合体前机身 前体分离涡 S弯进气道 大迎角 总压恢复系数 畸变指数
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大跨度异形吊杆钢拱桥的涡振性能
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作者 仝瑞金 杜文凯 +5 位作者 文锋 谢鹏飞 高广中 魏璟 赵勃隆 李加武 《兰州大学学报(自然科学版)》 北大核心 2025年第4期562-568,共7页
通过气弹模型风洞试验研究某大跨度拱桥的主拱圈和异形吊杆的抗风性能,确定主要构件涡激共振的发振风速和共振振幅,并改变原设计方案的阻尼和拱肋外形,研究其涡振性能.结果表明,全桥气弹模型实验中,风攻角在0°和3°时均出现小... 通过气弹模型风洞试验研究某大跨度拱桥的主拱圈和异形吊杆的抗风性能,确定主要构件涡激共振的发振风速和共振振幅,并改变原设计方案的阻尼和拱肋外形,研究其涡振性能.结果表明,全桥气弹模型实验中,风攻角在0°和3°时均出现小振幅的竖弯涡振现象,涡振发生在反对称竖弯振型,随着来流紊流的增加,涡振振幅减小.增加主拱圈的阻尼能够有效抑制其涡振响应.主拱圈断面的切角对涡振性能影响显著,带切角的断面外形具有更好的涡振性能.异形吊杆在高风速下出现面外涡振,振幅较小,最大振幅小于4.5 cm;面内涡振的振幅更小,起振风速更高. 展开更多
关键词 大跨度拱桥 异形吊杆 涡激共振 全桥气弹模型 风洞试验
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台阶壳体对诱导轮空化流动特性影响的数值研究
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作者 许啸雨 项乐 +2 位作者 陈晖 许开富 林荣浩 《应用力学学报》 北大核心 2025年第5期1016-1026,共11页
液体火箭发动机的可重复使用和大范围变推力对作为心脏部件的涡轮泵做功能力提出了极高的要求,诱导轮是决定涡轮泵抗空化能力的关键部件。空化流动特性对来流条件比较敏感,通过修改诱导轮入口壳体结构特征,可能有利于诱导轮空化性能的... 液体火箭发动机的可重复使用和大范围变推力对作为心脏部件的涡轮泵做功能力提出了极高的要求,诱导轮是决定涡轮泵抗空化能力的关键部件。空化流动特性对来流条件比较敏感,通过修改诱导轮入口壳体结构特征,可能有利于诱导轮空化性能的提升。采用先进的自适应空化模型对某典型三叶片诱导轮内空化流动特性进行数值仿真研究,首先基于可视化实验结果对数值仿真方法进行充分验证,发现采用的数值方法能够较好预测诱导轮内部空化形态和空化性能。基于数值仿真对匹配不同阶梯壳体的诱导轮内部空化流动特性进行深入分析,结果表明,扩张角为30°时的阶梯壳体性能最优,阶梯扩张使得诱导轮上游间隙增大,减弱了流体激振效应,在泄漏涡空化起始处,阶梯壳体形成类似回流涡的结构,对泄漏涡空化的涡心产生引导作用,导致空化区向上游发展,同时阶梯将空化区分割开,抑制了向下游发展的空化气泡,从而减小空化区对流道的堵塞和对相邻叶片入口冲角的干扰,进而提升诱导轮的空化性能并稳定了流道内流态。 展开更多
关键词 高速诱导轮 叶顶间隙泄漏涡空化 空化不稳定 阶梯壳体 空化模型
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射流孔形状对明渠中射流污染物输送扩散特性影响研究
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作者 杜富慧 玉潇楠 张士杰 《水电能源科学》 北大核心 2025年第11期63-67,共5页
为探究射流孔形状对横流中射流流动特性及稀释规律的影响,采用Realizable κ-ε湍流模型开展数值模拟,比较分析了圆形、正方形及多种矩形孔射流在横流作用下的速度分布、涡量沿程变化过程和浓度分布。结果表明,射流孔形状通过影响射流... 为探究射流孔形状对横流中射流流动特性及稀释规律的影响,采用Realizable κ-ε湍流模型开展数值模拟,比较分析了圆形、正方形及多种矩形孔射流在横流作用下的速度分布、涡量沿程变化过程和浓度分布。结果表明,射流孔形状通过影响射流初始动量分布及其与横流的相互作用机制进而影响射流的扩散特性。矩形孔直角边界诱导涡旋产生使得射流初始动量耗散,与圆形孔射流相比扩散效果更好。研究结果可为污水排放扩散器中射流孔形状的优化设计提供理论支持。 展开更多
关键词 射流 射流孔形状 流速分布 旋涡分布 扩散特性
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直线型和渐缩型喷嘴结构对涡流管性能的影响
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作者 劳有杰 王鹏飞 谢雍哲 《矿业工程研究》 2025年第2期56-65,共10页
采用FLUENT数值模拟软件,对喷嘴入口面积相同的圆形渐缩型、矩形渐缩型以及圆形直线型、矩形直线型这4种涡流管进行数值模拟.研究在压力为0.3,0.4,0.5 MPa条件下4种涡流管在0.5 MPa下的温度场、压力场和速度场分布.结果表明,矩形直线型... 采用FLUENT数值模拟软件,对喷嘴入口面积相同的圆形渐缩型、矩形渐缩型以及圆形直线型、矩形直线型这4种涡流管进行数值模拟.研究在压力为0.3,0.4,0.5 MPa条件下4种涡流管在0.5 MPa下的温度场、压力场和速度场分布.结果表明,矩形直线型喷嘴在0.5 MPa压力下具有最优的能量分离性能;矩形渐缩型喷嘴在各工作压力下均展现出稳定的制冷效果和较高的流动稳定性.进一步分析发现,渐缩型喷嘴因其压力分布更均匀、径向压力梯度更明显,有助于提升涡流管的制冷效率和工作稳定性. 展开更多
关键词 数值模拟 制冷效应 涡流管 喷嘴形状 压力场 速度场
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微型涡流发生器改善S弯喷管流场的实验研究
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作者 刘诗敏 梁华 +2 位作者 李金平 张富垚 马张煜 《推进技术》 北大核心 2025年第2期41-56,共16页
S弯喷管虽然能够提升飞行器隐身性能,但弯曲的几何结构会造成额外的总压损失和低能流体脉动增强的问题,导致飞行器性能降低,因此需要采用流动控制手段改善内部流场。本文将阵列式微型涡流发生器安装在S弯喷管上壁面中心线局部速度最大... S弯喷管虽然能够提升飞行器隐身性能,但弯曲的几何结构会造成额外的总压损失和低能流体脉动增强的问题,导致飞行器性能降低,因此需要采用流动控制手段改善内部流场。本文将阵列式微型涡流发生器安装在S弯喷管上壁面中心线局部速度最大点前侧,研究其在冷态流场中对喷管出口总压损失的控制效果和对上壁面下游流场低频脉动的抑制效果。结果表明:(1)在试验参数下,对于相同高度的微型涡流发生器,安装位置距离局部速度最大点较远时,喷管出口截面总压损失系数更低。(2)落压比为1.2时,安装高度为2.2%喷管入口直径的微型涡流发生器,能够使喷管出口平均总压损失系数相对基准降低8.57%。(3)微型涡流发生器能降低喷管上壁面下游流场的低频脉动,使脉动幅值降低22.8%,提升低能流稳定性。 展开更多
关键词 S弯喷管 微型涡流发生器 总压损失 流动控制 变分模态分解
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悬挑人行道对π型叠合梁涡振的影响及气动措施优化风洞试验研究
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作者 黄钰婵 陈强草 +2 位作者 陈富军 李高鹏 温青 《世界桥梁》 北大核心 2025年第2期66-72,共7页
为研究悬挑人行道对π型断面钢-混叠合梁(简称π型叠合梁)涡振性能的影响、优化悬挑人行道布置位置和气动措施,以某大跨π型叠合梁斜拉桥为背景,开展无悬挑人行道和3种带悬挑人行道的π型叠合梁节段模型风洞试验,对比分析悬挑人行道对... 为研究悬挑人行道对π型断面钢-混叠合梁(简称π型叠合梁)涡振性能的影响、优化悬挑人行道布置位置和气动措施,以某大跨π型叠合梁斜拉桥为背景,开展无悬挑人行道和3种带悬挑人行道的π型叠合梁节段模型风洞试验,对比分析悬挑人行道对主梁涡振性能的影响,对下稳定板抑振气动措施进行优化。结果表明:π型叠合梁极易发生竖向涡振,在主梁两侧增加悬挑人行道可以有效减小π型叠合梁的涡振振幅;随着悬挑人行道板和桥面板之间的高差增大,主梁涡振振幅随之减小,悬挑人行道越靠近主纵梁中部,抑振效果越好;下稳定板气动措施可以有效抑制带悬挑人行道π型叠合梁的竖向涡振,两侧稳定板气动措施的抑振效果优于中央稳定板,可使涡振几乎消失。 展开更多
关键词 斜拉桥 π型叠合梁 涡振 悬挑人行道 下稳定板 风洞试验
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