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Generating Entangled Pairs of Vortex Photons via Induced Emission
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作者 D.V.Grosman G.K.Sizykh +2 位作者 E.O.Lazarev G.V.Voloshin D.V.Karlovets 《Chinese Physics Letters》 2025年第12期115-125,共11页
Pairs of entangled vortex photons can promise new prospects of application in quantum computing and cryptography.We investigate the possibility of generating such states via two-level atom emission induced by a single... Pairs of entangled vortex photons can promise new prospects of application in quantum computing and cryptography.We investigate the possibility of generating such states via two-level atom emission induced by a single photon wave packet with a definite total angular momentum(TAM).The entangled pair produced in this process possesses well-defined mean TAM with the TAM variation being much smaller than h.On top of that,the variation exponentially decreases with the increase in TAM of the incident photon.Our model allows one to track the time evolution of the state of the entangled pair.An experimentally feasible scenario is assumed,in which the incident photon interacts with a spatially confined atomic target.We conclude that induced emission can be used as a source of entangled vortex photons with applications in atomic physics experiments,quantum optics,and quantum information sciences. 展开更多
关键词 entangled vortex photons total angular momentum tam incident photonour entangled pair quantum computing photon wave vortex photons entangled photons
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Effects of initial electronic state on vortex patterns in counter-rotating circularly polarized attosecond pulses
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作者 Qi Zhen Jia-He Chen +2 位作者 Si-Qi Zhang Zhi-Jie Yang Xue-Shen Liu 《Chinese Physics B》 SCIE EI CAS CSCD 2021年第2期293-297,共5页
We theoretically investigate the effects of different electronic states as the initial state on the vortex patterns in photoelectron momentum distributions(PMDs)from numerical solutions of the two-dimensional(2D)time-... We theoretically investigate the effects of different electronic states as the initial state on the vortex patterns in photoelectron momentum distributions(PMDs)from numerical solutions of the two-dimensional(2D)time-dependent Schrodinger equation(TDSE)of He^(+)with a pair of counter-rotating circularly polarized attosecond pulses.It is found that the number of spiral arms in vortex patterns is equal to the number of the absorbed photons when the initial state is the ground state.However,the number of spiral arms in vortex patterns is always two more than the number of the absorbed photons when the initial state is the excited state.This sensitivity is attributed to the initial electron density distribution.In addition,we have demonstrated the PMDs for different initial electronic states with the same wavelengths and analyzed their corresponding physical mechanisms.It is illustrated that the method presented can be employed to effectively control the distribution of the electron vortices. 展开更多
关键词 initial electronic state counter-rotating circularly polarized attosecond pulses vortex patterns photoelectron momentum distributions
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Planar laser scattering visualization of streamwise vortex pairs in a Mach 6 flow 被引量:2
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作者 Yinkai MA Zhufei LI Jiming YANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2023年第1期166-177,共12页
A series of cross-sectional flow fields of Counterrotating Vortex Pairs(CVPs) generated by a large-scale ramp vortex generator is observed using an ice-cluster-based Planar Laser Scattering(PLS) method in a shock tunn... A series of cross-sectional flow fields of Counterrotating Vortex Pairs(CVPs) generated by a large-scale ramp vortex generator is observed using an ice-cluster-based Planar Laser Scattering(PLS) method in a shock tunnel with a nominal flow Mach number of 6. Combined with a numerical simulation, two streamwise CVPs with opposite rotating directions are identified in the wake flow of the vortex generator with an absence of a boundary layer, namely, a Primary CVP(PCVP) and a Secondary CVP(SCVP). The wake flow is divided into two stages with different features of the PCVP and SCVP. In Stage Ⅰ, the PCVP and SCVP gradually mature, and the flow is relatively stable. In Stage Ⅱ, the PCVP and SCVP depart from each other, and the flow becomes unstable. The profiles of the transverse velocity in the spanwise symmetry plane induced by the PCVP and SCVP do not obey the scaling law of CVPs immersed in the boundary layer. A new scaling law is proposed, in which the transverse distances between adjacent saddle points in the cross-sectional flow field are used as the characteristic lengths for the PCVP and SCVP. After this new scaling procedure, the profiles of transverse velocity induced by the PCVP and SCVP at different streamwise locations collapse well. Moreover, the PLS images show that the mixing between the CVPs and the outside high-momentum flow becomes evident at approximately 5.5 times the height of the vortex generator, which is earlier than that immersed in the boundary layer. These findings enrich the knowledge of CVPs in the hypersonic regime, especially in the absence of the boundary layer. 展开更多
关键词 Counterrotating vortex pair Hypersonic flow Planar laser scattering Scaling law Shock tunnel
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Tomographic particle image velocimetry measurement on three-dimensional swirling flow in dual-stage counter-rotating swirler 被引量:2
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作者 Yuyang ZHOU Ling DONG +2 位作者 Mingtao SHANG Jibao LI Akira RINOSHIKA 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2024年第3期7-20,共14页
Three-Dimensional(3D)swirling flow structures,generated by a counter-rotating dualstage swirler in a confined chamber with a confinement ratio of 1.53,were experimentally investigated at Re=2.3×10^(5)using Tomogr... Three-Dimensional(3D)swirling flow structures,generated by a counter-rotating dualstage swirler in a confined chamber with a confinement ratio of 1.53,were experimentally investigated at Re=2.3×10^(5)using Tomographic Particle Image Velocimetry(Tomo-PIV)and planar Particle Image Velocimetry(PIV).Based on the analysis of the 3D time-averaged swirling flow structures and 3D Proper Orthogonal Decomposition(POD)of the Tomo-PIV data,typical coherent flow structures,including the Corner Recirculation Zone(CRZ),Central Recirculation Zone(CTRZ),and Lip Recirculation Zone(LRZ),were extracted.The counter-rotating dual-stage swirler with a Venturi flare generates the independence process of vortex breakdown from the main stage and pilot stage,leading to the formation of an LRZ and a smaller CTRZ near the nozzle outlet.The confinement squeezes the CRZ to the corner and causes a reverse rotation flow to limit the shape of the CTRZ.A large-scale flow structure caused by the main stage features an explosive breakup,flapping,and Precessing Vortex Core(PVC).The explosive breakup mode dominates the swirling flow structures owing to the expansion and construction of the main jet,whereas the flapping mode is related to the wake perturbation.Confinement limits the expansion of PVC and causes it to contract after the impacting area. 展开更多
关键词 Coherent structures Dual-stage counter-rotating swirler cup Precessing vortex core Proper orthogonal decomposition Swirling flow Tomographic particle image velocimetry
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Low-Frequency Vortex Pair over the Tropical Eastern Indian Ocean and the South China Sea Summer Monsoon Onset 被引量:1
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作者 PAN Jing LI Chong-Yin 《Atmospheric and Oceanic Science Letters》 2011年第6期304-308,共5页
In this paper,the relationship between a pair of low-frequency vortexes over the equatorial Indian Ocean and the South China Sea(SCS) summer monsoon onset is studied based on a multi-year(1980-2003) analysis.A pair of... In this paper,the relationship between a pair of low-frequency vortexes over the equatorial Indian Ocean and the South China Sea(SCS) summer monsoon onset is studied based on a multi-year(1980-2003) analysis.A pair of vortexes symmetric about the equator is an important feature prior to the SCS summer monsoon onset.A composite analysis shows that the life cycle of the pair of vortexes is closely associated with the SCS summer monsoon onset.The westerly between the twin cyclones is an important factor to the SCS summer monsoon onset process. 展开更多
关键词 oscillation low-frequency vortex pair intra-seasonal South China Sea summer monsoon onset
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Tight Focusing Properties of Azimuthally Polarized Pair of Vortex Beams through a Dielectric Interface 被引量:1
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作者 C. A. P. Janet M. Lavanya +3 位作者 K. B. Rajesh M. Udhayakumar Z. Jaroszewicz D. Velauthapillai 《Chinese Physics Letters》 SCIE CAS CSCD 2017年第7期109-113,共5页
Tight focusing properties of an azimuthally polarized Gaussian beam with a pair of vortices through a dielectric interface is theoretically investigated by vector diffraction theory. For the incident beam with a pair ... Tight focusing properties of an azimuthally polarized Gaussian beam with a pair of vortices through a dielectric interface is theoretically investigated by vector diffraction theory. For the incident beam with a pair of vortices of opposite topological charges, the vortices move toward each other, annihilate and revive in the vicinity of focal plane, which results in the generation of many novel focal patterns. The usable focal structures generated through the tight focusing of the double-vortex beams may find applications in micro-particle trapping, manipulation, and material processing, etc. 展开更多
关键词 Tight Focusing Properties of Azimuthally Polarized pair of vortex Beams through a Dielectric Interface
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ON THE FORMATION OF VORTEX RINGS AND PAIRS
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作者 赵耀 王健平 是勋刚 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1998年第2期113-129,共7页
The axisymmetric vortex sheet model developed by Nitsche and Krasny had been extended to study the formation of vortex rings (pairs) at the edge of circular (2D) tube and opening. Computations based on this model wer... The axisymmetric vortex sheet model developed by Nitsche and Krasny had been extended to study the formation of vortex rings (pairs) at the edge of circular (2D) tube and opening. Computations based on this model were in good agreement with the experiments (Didden (1979) for circular tube and Auerbach (1987) for 2D tube and opening). Using this new model, evidences are provided to show that the main failure of the similarity theory (the false prediction of axial trajectory of vortex ring) is due to its ignorance of the self-induced ring velocity (mutual induction for vortex pair). The Glezer (1988)'s summary on the influence of piston speed upon the shedding circulation was also discussed, and finally the variation of core distribution of vortex ring with turning angle and piston speed was given. (Edited author abstract) 22 Refs. 展开更多
关键词 formation of vortex ring (pair) vortex method the similarity theory
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Dynamics of vortex–antivortex pair in a superconducting thin strip with narrow slits
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作者 何安 薛存 周又和 《Chinese Physics B》 SCIE EI CAS CSCD 2017年第4期449-456,共8页
In the framework of phenomenological time-dependent Ginzburg-Landau(TDGL) formalism,the dynamical properties of vortex-antivortex(V-Av) pair in a superconductor film with a narrow slit was studied.The slit positio... In the framework of phenomenological time-dependent Ginzburg-Landau(TDGL) formalism,the dynamical properties of vortex-antivortex(V-Av) pair in a superconductor film with a narrow slit was studied.The slit position and length can have a great impact not only on the vortex dynamical behavior but also the current-voltage(Ⅰ-Ⅴ) characteristics of the sample.Kinematic vortex lines can be predominated by the location of the slit.In the range of relatively low applied currents for a constant weak magnetic field,kinematic vortex line appears at right or left side of the slit by turns periodically.We found such single-side kinematic vortex line cannot lead to a jump in the Ⅰ-Ⅴ curve.At higher applied currents the phase-slip lines can be observed at left and right sides of the slit simultaneously.The competition between the vortex created at the lateral edge of the sample and the V-Av pair in the slit will result in three distinctly different scenarios of vortex dynamics depending on slit length:the lateral vortex penetrates the sample to annihilate the antivortex in the slit;the V-Av pair in the slit are driven off and expelled laterally;both the lateral vortex and the slit antivortex are depinned and driven together to annihilation in the halfway. 展开更多
关键词 vortex-antivortex pair phase-slip line current-voltage characteristic narrow slit
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Vortex structure simulation for supersonic mixing layers using nonlinear PSE method
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作者 Xin Guo Qiang Wang 《Theoretical & Applied Mechanics Letters》 2012年第3期53-56,共4页
The method of nonlinear parabolized stability equations(PSE) is applied in the simulation of vortex structures in compressible mixing layer.The spatially-evolving unstable waves,which dominate the vortex structure,a... The method of nonlinear parabolized stability equations(PSE) is applied in the simulation of vortex structures in compressible mixing layer.The spatially-evolving unstable waves,which dominate the vortex structure,are investigated through spatial marching method.The instantaneous flow field is obtained by adding the harmonic waves to basic flow.The results show that T-S waves do not keep growing exponentially as the linear evolution,the energy transfer to high order harmonic modes,and that finally all harmonic modes get saturated due to nonlinear interaction.The mean flow distortion induced by the nonlinear interaction between the harmonic modes and their conjugate harmonic ones,makes great change of the average flow and increases the thickness of mixing layer. PSE methods can well capture the two- and three-dimensional large scale nonlinear vortex structures in mixing layers such as vortex roll-up,vortex pairing,and A vortex. 展开更多
关键词 compressible mixing layer parabolized stability equations nonlinear stability vortex rollup vortex pairing A vortex
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横流中射流水动力与声学性能数值模拟研究
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作者 张博艺 靳国永 +2 位作者 叶天贵 宋晓济 靳淼 《船舶力学》 北大核心 2025年第4期669-679,共11页
水下航行器舷外排放形成了横流与射流相互作用的流体结构,横流中射流产生的流体动力学特性是流体领域的重要课题。本文基于雷诺平均与大涡模拟方法,建立横流中射流的数值计算模型,将时均速度与脉动压力结果与文献试验结果进行对比,验证... 水下航行器舷外排放形成了横流与射流相互作用的流体结构,横流中射流产生的流体动力学特性是流体领域的重要课题。本文基于雷诺平均与大涡模拟方法,建立横流中射流的数值计算模型,将时均速度与脉动压力结果与文献试验结果进行对比,验证计算方法的准确性。基于数值计算结果探究孔口上下游近壁面速度及涡量特性,分析孔口附近的声场特性。结果表明:孔口射流对上游边界层的影响体现在前6倍孔径范围内,孔口下游2~14倍孔径范围内发生流动分离;在横流与射流干涉作用下,孔口下游形成了反对称涡对的特征涡结构;反旋对称涡对形成于孔口下边缘附近,并在下游持续存在,其涡核沿流向距离增加逐渐远离壁面,影响区域逐渐扩大;横流与射流相互作用产生的主要声源位于壁面附近,孔口附近声源水平较高且存在脱离壁面的特征,孔口下游声压水平明显高于孔口上游相同位置,声场辐射与流向相关,存在明显的指向性特征。 展开更多
关键词 射流注入横流 边界层特性 特征涡结构 反旋对称涡对 涡声方程
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偏置对涡畸变与风扇耦合影响机理研究
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作者 陈奇 黄国平 +1 位作者 刘泽鹏 张洪鑫 《航空动力学报》 北大核心 2025年第6期360-372,共13页
根据典型大S弯进气道出口偏置对涡畸变的速度、压力分布特征,利用涡团模型建立了一种偏置对涡边界条件定义方法,并进行数值模拟研究探索了偏置对涡畸变与风扇的耦合影响机理。研究结果表明:在风扇吸力作用下,上游畸变流掺混加强,切向速... 根据典型大S弯进气道出口偏置对涡畸变的速度、压力分布特征,利用涡团模型建立了一种偏置对涡边界条件定义方法,并进行数值模拟研究探索了偏置对涡畸变与风扇的耦合影响机理。研究结果表明:在风扇吸力作用下,上游畸变流掺混加强,切向速度增大。偏置对涡进气条件会使风扇性能下降,稳定裕度损失严重,其中在涡旋环量35 m2/s相斥对涡进气条件下风扇稳定裕度损失7.1%,相吸对涡进气条件下稳定裕度损失达到了7.9%。随着偏置对涡强度的增大,风扇性能下降更多,稳定裕度损失也更大。偏置对涡进气条件下风扇轴向速度损失以及切向预旋造成的风扇叶尖出现大范围大攻角区,造成风扇部分叶片通道压比较大,而风扇其余位置仍处于较低压比水平,导致近失速点附近风扇整体总压比下降,失速点提前。 展开更多
关键词 耦合影响机理 大S弯进气道 进气道/发动机匹配 偏置对涡畸变 涡团模型 风扇失速
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Tomography-like flow visualization of a hypersonic inward-turning inlet 被引量:9
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作者 Yiming LI Zhufei LI Jiming YANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2021年第1期44-49,共6页
The flow field in a typical inward-turning inlet was visualized using the Planar Laser Scattering(PLS)method in a shock tunnel with a nominal Mach number of 6.The opaque inlet,which is truncated at a series of section... The flow field in a typical inward-turning inlet was visualized using the Planar Laser Scattering(PLS)method in a shock tunnel with a nominal Mach number of 6.The opaque inlet,which is truncated at a series of sections,and the following transparent isolator,are combined to enable the optical access at different streamwise locations.The sequential PLS images provide a tomography-like flow visualization,which confirm the existence of streamwise Counter-rotating Vortex Pairs(CVPs)in both external and internal flow field of the inlet.Generation mechanisms of these CVPs are unraveled with the help of a numerical simulation,among which the cowl notch plays an important role in the generation of surface trailing CVPs along the centerline of the cowl.Moreover,the cowl shock sweeps the internal boundary layer towards the body side,which ultimately accumulates low-momentum flow on the body side in forms of a large CVP propagating downstream through the isolator.The CVPs formed in the shape-transition are responsible for the nonuniform flow field of the inward-turning inlet.This study indicates that the V-shaped cowl notch affects the downstream flow significantly and,therefore,should be examined thoroughly in practical applications. 展开更多
关键词 counter-rotating vortex pair(CVP) Flow visualization Inward-turning inlet Planar Laser Scattering(PLS)method Shock wave
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南海夏季风爆发的环流特征及指标研究 被引量:44
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作者 张秀芝 李江龙 +1 位作者 闫俊岳 丁一汇 《气候与环境研究》 CSCD 2002年第3期321-331,共11页
使用美国NCEP/NCAR高度场和风场资料及外逸长波辐射(OLR)资料,分析了4~7月南亚和东亚上空环流场,给出了南海夏季风爆发的定义及1953~1999年季风爆发的时间序列,指出季风爆发存在3种类型的环流场,发现东印度洋赤道两侧涡旋对的出现... 使用美国NCEP/NCAR高度场和风场资料及外逸长波辐射(OLR)资料,分析了4~7月南亚和东亚上空环流场,给出了南海夏季风爆发的定义及1953~1999年季风爆发的时间序列,指出季风爆发存在3种类型的环流场,发现东印度洋赤道两侧涡旋对的出现对季风爆发有很好的指示意义。综合季风爆发过程中热力学和动力学要素的特征,建立了适合南海夏季风爆发的指数计算经验公式。 展开更多
关键词 南海 夏季风 环流场 涡旋对 爆发指标 外逸长波辐射 热力学 动力学
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合成射流作用机理及其对共轴射流掺混的影响 被引量:7
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作者 刘艳明 伍耐明 +1 位作者 董金钟 周盛 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2007年第1期5-9,共5页
对合成射流流场及其作用下的内、外涵共轴射流流场进行了二维非定常数值模拟,研究了合成射流流场和共轴射流流场情况.结果表明,合成射流由一系列对称分布在中心线2侧的旋涡对组成,频率与激振频率相同,对外场构成一扰动力;涡对自形成后... 对合成射流流场及其作用下的内、外涵共轴射流流场进行了二维非定常数值模拟,研究了合成射流流场和共轴射流流场情况.结果表明,合成射流由一系列对称分布在中心线2侧的旋涡对组成,频率与激振频率相同,对外场构成一扰动力;涡对自形成后向远处运移速基本稳定;腔内和腔外涡对的形成及发展变化过程总体保持一致,在每时刻则呈现截然相反的发展态势;中心线速度的降幅起伏变化分布是由激励器的激振变化引起的,体现了涡量产生、发展变化的基本特征;合成射流激励器的采用可使共轴射流截面掺混率比未加激励时得到增加,增强了共轴射流的掺混效果. 展开更多
关键词 合成射流 涡对 剪切应力 混合
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超声速平面混合层小激波的形成与演变 被引量:6
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作者 张焕好 陈志华 +1 位作者 黄振贵 姜孝海 《计算力学学报》 EI CAS CSCD 北大核心 2012年第5期772-778,共7页
为了揭示超声速混合层中小激波形成机理及其与涡相互作用的演变过程,本文基于大涡模拟(LES)方法,结合五阶精度混合TCD/WENO格式,对超声速平面混合层在对流马赫数为Mc=0.65条件下的流场结构进行了数值模拟,数值结果详细描述了超声速混合... 为了揭示超声速混合层中小激波形成机理及其与涡相互作用的演变过程,本文基于大涡模拟(LES)方法,结合五阶精度混合TCD/WENO格式,对超声速平面混合层在对流马赫数为Mc=0.65条件下的流场结构进行了数值模拟,数值结果详细描述了超声速混合层中小激波的形成过程。研究了小激波形成后,随涡运动而产生的变形、脱落及发展过程。同时,对混合层双涡合并过程中,小激波与相邻涡相互作用所产生的变形与演变过程进行了讨论。 展开更多
关键词 超声速混合层 小激波 可压缩性 大涡模拟 双涡合并
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利用W型槽提高气膜冷却效率机理 被引量:12
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作者 李广超 陈钰恺 +2 位作者 刘永泉 杜治能 张魏 《推进技术》 EI CAS CSCD 北大核心 2016年第3期520-526,共7页
为了探讨圆柱孔出口开有W型槽结构的气膜冷却机理,数值模拟研究了W型槽与横向槽下游流场、温度场及气膜冷却效率。分析了W型槽深度对气膜冷却效率的影响。结果表明:相比于横向槽,W型槽结构展向平均气膜冷却效率提高70%~130%。随着W型... 为了探讨圆柱孔出口开有W型槽结构的气膜冷却机理,数值模拟研究了W型槽与横向槽下游流场、温度场及气膜冷却效率。分析了W型槽深度对气膜冷却效率的影响。结果表明:相比于横向槽,W型槽结构展向平均气膜冷却效率提高70%~130%。随着W型槽深度增加,气膜孔出口下游的对漩涡减弱,两侧的附加漩涡增强,最终形成一对反向对漩涡。小吹风比0.5时,三种W型槽深结构的展向平均气膜冷却效率差别小于8%;大吹风比1.5时,槽深0.5D(D为气膜孔孔径)结构展向平均气膜冷却效率高于槽深0.25D结构的展向平均气膜冷却效率75%~150%。槽深0.5D和0.75D结构的展向平均气膜冷却效率基本相同,差别小于3%。 展开更多
关键词 涡轮叶片 薄膜冷却 冷却效率 涡对 W型槽
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涡方法分析并列圆柱的旋涡脱落现象 被引量:12
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作者 周志勇 陈艾荣 项海帆 《空气动力学学报》 CSCD 北大核心 2003年第1期38-46,共9页
利用快速离散涡方法及流场可视化技术分析二维粘性不可压缩均匀流中并列圆柱体的旋涡脱落现象,识别作用在圆柱上的气动力及旋涡脱落频率。使用边界元方法及引入一个新颍的涡量边界条件计算表面涡量,利用系数影响矩阵技术获得无网格方法... 利用快速离散涡方法及流场可视化技术分析二维粘性不可压缩均匀流中并列圆柱体的旋涡脱落现象,识别作用在圆柱上的气动力及旋涡脱落频率。使用边界元方法及引入一个新颍的涡量边界条件计算表面涡量,利用系数影响矩阵技术获得无网格方法,采用自适应快速多极子算法快速计算涡元速度。数值算例再现了不同间距并列圆柱体的同步同相旋涡脱落、同步反相旋涡脱落、尾流的不对称性及间隙流的半稳定性等现象,数值结果与早期实验结果吻合得很好。 展开更多
关键词 离散涡方法 涡量边界条件 并列圆柱 旋涡脱落
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基于PANS模型的水翼非定常空化特性研究 被引量:7
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作者 施卫东 张光建 张德胜 《华中科技大学学报(自然科学版)》 EI CAS CSCD 北大核心 2014年第4期1-5,10,共6页
采用一种局部时均化模型(PANS)对绕二维Clark-y型水翼的空化流动进行数值计算.分别研究了空化模型中最大密度比对空化计算的影响,PANS模型中关键控制参数fk对云空化非定常特性的影响和云空化阶段空泡形态及升力系数随时间的演变,并与实... 采用一种局部时均化模型(PANS)对绕二维Clark-y型水翼的空化流动进行数值计算.分别研究了空化模型中最大密度比对空化计算的影响,PANS模型中关键控制参数fk对云空化非定常特性的影响和云空化阶段空泡形态及升力系数随时间的演变,并与实验结果进行对比.结果表明:最大密度比会影响液相与气相之间的质量传递速率,将最大密度比提高,可大大改善数值预测的精度;随着fk值的减小,PANS模型可释放更多的湍流尺度,较好地预测云空化中强烈的非定常特性;由于云空化呈现出产生-发展-脱落-溃灭的准周期性变化,使得水翼的升力系数变化剧烈,计算出时均升力系数为0.708,与实验值0.760相差约7%;回射流与主流相互作用,在水翼尾部形成的一对旋转方向相反的旋涡是云状空泡形成与发展的主要原因. 展开更多
关键词 空化流 水翼 湍流模型 空化模型 回射流 旋涡对
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一种平面埋入式进气道的地面工作特性及流态特征 被引量:8
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作者 孙姝 郭荣伟 伍贻兆 《航空动力学报》 EI CAS CSCD 北大核心 2007年第3期390-395,共6页
对一种平面埋入式进气道的地面工作特性进行了实验研究,结合数值仿真技术,分析了地面工作状态下该类进气道的流态特征,并探讨了其出口总压图谱的形成成因.结果表明:(1)虽然进气道出口截面的二次流较弱,但通道内却存在强的以对涡为特征... 对一种平面埋入式进气道的地面工作特性进行了实验研究,结合数值仿真技术,分析了地面工作状态下该类进气道的流态特征,并探讨了其出口总压图谱的形成成因.结果表明:(1)虽然进气道出口截面的二次流较弱,但通道内却存在强的以对涡为特征的旋流,该对涡因埋入式进气道进口侧棱的存在而产生,与后唇口前缘的气流分离共同导致了进气道出口截面的大面积低总压区;(2)地面工作状态下,埋入式进气道的总压恢复系数随出口马赫数的上升而下降,周向畸变指数、紊流度和综合畸变指数则随着出口马赫数的增加而增加.在相同的出口马赫数下,地面工作状态的总压恢复系数高于飞行状态,各种畸变指数也明显偏高.但当发动机的进口工作马赫数为0.35左右时,进气道出口截面的综合畸变指数W小于10.0%,满足常规发动机的稳定工作要求;(3)计算和实验结果对比表明,所得到的进气道出口总压恢复系数相对误差在1.2%以内,但畸变指数整体偏大. 展开更多
关键词 航空 航天推进系统 平面埋入式进气道 地面工作状态 对涡 总压恢复系数
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大小孔交替排列对气膜冷却效率的影响 被引量:7
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作者 刘晓红 罗翔 陶智 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2010年第11期1271-1274,1280,共5页
采用数值模拟方法研究了大小气膜孔交替排列(均匀排列的圆柱形单孔两侧分别开设一个平行的小孔)情况下的流动和换热,并与常规的圆柱形单孔结构进行对比,分析大小气膜孔交替排列提高冷效的机理,研究大小孔的孔径比对气膜冷却效果的影响规... 采用数值模拟方法研究了大小气膜孔交替排列(均匀排列的圆柱形单孔两侧分别开设一个平行的小孔)情况下的流动和换热,并与常规的圆柱形单孔结构进行对比,分析大小气膜孔交替排列提高冷效的机理,研究大小孔的孔径比对气膜冷却效果的影响规律.结果发现:在圆柱形单孔两侧分别设置一个平行的辅助小孔,大小孔冷气射流的肾形涡相互干涉,导致主气膜孔下游的肾形涡的尺度和强度与圆柱形单孔相比均有明显降低,气膜冷却效果明显改善.相同冷气量下,小孔孔径越大,分配的冷气流量越大,对主孔冷气射流的干涉作用越强,气膜冷却效果改善越明显;当小孔孔径d2=4mm时,气膜冷却结构类似常规的离散圆柱形气膜孔,气膜冷却效果开始下降. 展开更多
关键词 气膜冷却 绝热冷效 射流 肾形涡
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