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Spark-generated bubble collapse near or inside a circular aperture and the ensuing vortex ring and droplet formation 被引量:7
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作者 Abdolrahman Dadvand Mazyar Dawoodian +1 位作者 Boo Cheong Khoo Reza Esmaily 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2013年第5期657-666,共10页
This paper aims to study the oscillation of a sparkgenerated submerged bubble located near or inside a circular aperture made in a flat plate using high-speed visualization technique. In the case of a bubble oscillati... This paper aims to study the oscillation of a sparkgenerated submerged bubble located near or inside a circular aperture made in a flat plate using high-speed visualization technique. In the case of a bubble oscillating near an aperture the initial free surface of the water was set at the bottom surface of the plate. The effects of aperture size and bubblefree surface distance on the bubble behavior as well as on the ensuing droplet dynamics are investigated. It was found that the direction of the bubble reentrant jet was towards the aperture or away from it respectively when the normalized aperture size was smaller or greater than a certain critical value. In addition, a toroidal vortex ring was observed to form, which rotated inwards as it moved away from the aperture. It was also found that if the bubble was incepted at a distance sufficiently away from a supercritical size aperture a single droplet could be produced. In the case of a bub- ble initiated in the middle of a circular aperture submerged just beneath the water free surface, the bubble was found to take the shape of an ellipsoid during its expansion. Then a reentrant jet was initiated and pierced the bubble from its top side. 展开更多
关键词 Spark bubble Toroidal bubble vortex ring Droplet formation High-speed video camera
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Passive scalar mixing induced by the formation of compressible vortex rings 被引量:2
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作者 Haiyan Lin Yang Xiang +2 位作者 Hui Xu Hong Liu Bin Zhang 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2020年第6期1258-1274,I0003,共18页
This study aims to determine the relationship between the physical features of a compressible vortex and the mixing process.Such relationship is of significant importance to design combustors that can achieve optimal ... This study aims to determine the relationship between the physical features of a compressible vortex and the mixing process.Such relationship is of significant importance to design combustors that can achieve optimal or most effective mixing.The passive scalar mixing induced by the formation of a canonical compressible vortex ring(CVR)generated at the end of a shock tube is investigated by using numerical simulation.In addition,the method of finite-time Lyapunov exponent(FTLE)field are detected to identify the region of CVR,as well as to analyze the passive scalar mixing during the CVR formation.As the CVR rolls up,the ambient fluid outside the shock tube is entrained into the ring.The entrainment fraction(the mass of entrained fluid to the total mass of CVR)is found to strongly depend on two features of CVRs.One is the compressibility of CVRs,which is characterized by the Mach number of the incident shock denoted by Mach number(Ma).The other is pinch-off of CVRs,which happens at a certain timescale with narrow range of 2–4.As Ma increases,the entrainment fraction of the leading CVR decreases linearly due to smaller vortex core and weaker radial diffusion of vorticity generated by larger compressibility.After CVRs pinch off,trailing vortices appear and show less effective at entrainment than the leading CVRs do.Moreover,the tendency of the rate of entrainment is examined.The results indicate that increasing compressibility and total fluid flux are in favor of the rate of entrainment but restrain the entrainment fraction of total jet. 展开更多
关键词 vortex ring Finite-time Lyapunov exponent(FTLE) ENTRAINMENT PINCH-OFF
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A PREDICTION OF THE VORTEX-RING STATE BOUNDARY BASED ON MODEL TESTS 被引量:3
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作者 Xin Hong Gao Zheng(Department of Aircraft Engineering,NUAA 29 Yudao Street,Nanjing 210016,P.R.China) 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 1994年第2期159-164,共6页
To understand the vortex-ring state and to develop an approach for predicting its boundary, a series of model rotor tests of vertical descent and oblique descent have been conducted on a newly-built test apparatus - t... To understand the vortex-ring state and to develop an approach for predicting its boundary, a series of model rotor tests of vertical descent and oblique descent have been conducted on a newly-built test apparatus - the Whirling Beam. The test results showed some unsteady aerodynamic behavior of the model rotor operating in the vortex-ring state. A very irregular variation of the rotortorque at low rate-of-descent was observed here for the first time. We considered it to be the start of the 'power settling' and determined the critical descent velocity according to this observation. A previous criterion for the vortex-ring state was modified to give a semi-empirical method for predicting the entire vortex-ring state boundary. The computed boundary shows a good correlation with the model test results and the flight experiences. 展开更多
关键词 helicopters ROTOR WINGS AERODYNAMICS model tests vortex-ring STATE
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Lagrangian analysis of the formation and mass transport of compressible vortex rings generated by a shock tube 被引量:2
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作者 Haiyan Lin Yang Xiang +1 位作者 Hong Liu Bin Zhang 《Chinese Physics B》 SCIE EI CAS CSCD 2021年第3期183-193,共11页
In order to understand the mass transport and the dynamic genesis associated with a compressible vortex formation,a dynamic analysis of compressible vortex rings (CVRs) generated by shock tubes by using the framework ... In order to understand the mass transport and the dynamic genesis associated with a compressible vortex formation,a dynamic analysis of compressible vortex rings (CVRs) generated by shock tubes by using the framework of Lagrangiancoherent structures (LCSs) and finite-time Lyapunov exponents field (FTLE) is performed. Numerical calculation is performed to simulate the evolution of CVRs generated by shock tubes with 70 mm, 100 mm, and 165 mm of the driver sectionat the circumstances of pressure ratio = 3. The formation of CVRs is studied according to FTLE fields. The mass transportduring the formation is obviously seen by the material manifold reveled by FTLE fields. A non-universal formation numberfor the three CVRs is obtained. Then the elliptic LCSs is implemented on three CVRs. Fluid particles separated by ellipticLCSs and ridges of FTLE are traced back to t = 0 to identify the fluid that eventually forms the CVRs. The elliptic LCSsencompass around 60% fluid material of the advected bulk but contain the majority of the circulation of the ring. The otherparts of the ring carrying almost zero circulation advect along with the ring. Combining the ridges of FTLE and the ellipticLCS, the whole CVR can be divided into three distinct dynamic parts: vortex part, entrainment part, and advected part. Inaddition, a criterion based on the vortex part formation is suggested to identify the formation number of CVRs. 展开更多
关键词 compressible vortex rings Lagrangian coherent structure mass transport
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Large eddy simulation of a vortex ring impinging on a three-dimensional circular cylinder 被引量:1
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作者 Heng Ren Xiyun Lu 《Theoretical & Applied Mechanics Letters》 CAS 2013年第3期46-50,共5页
Abstract A vortex ring impacting a three-dimensional circular cylinder is studied using large eddy simulation (LES) for a Reynolds number Re = 4 × 10^4 based on the initial translation speed and diameter of the... Abstract A vortex ring impacting a three-dimensional circular cylinder is studied using large eddy simulation (LES) for a Reynolds number Re = 4 × 10^4 based on the initial translation speed and diameter of the vortex ring. We have investigated the evolution of vortical structures and identified three typical evolution phases. When the primary vortex closely approaches to the cylinder, a secondary vortex is generated and its segment parts move inward to the primary vortex ring. Then two large-scale loop-like vortices are formed to evolve in opposite directions. Thirdly, the two loop-like vortices collide with each other to form complicated small-scale vortical structures. Moreover, a series of hair-pin vortices are generated due to the stretching and deformation of the tertiary vortex. The trajectories of vortical structures and the relevant evolution speeds are analyzed. The total kinetic energy and enstrophy are investigated to reveal their properties relevant to the three evolution phases. 展开更多
关键词 large eddy simulation vortex ring circular cylinder vortical structure high Reynoldsnumber
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THE NONLINEAR INTERACTION OF VORTEX RINGS WITH A FREE SURFACE
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作者 叶取源 C.K.Chu 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1997年第2期120-129,共10页
Nonlinear interactions of vortex rings with a free surface are considered in an incompressible, ideal fluid using the vortex contour dynamics technique and the boundary integral equation method. The flow is axisymmetr... Nonlinear interactions of vortex rings with a free surface are considered in an incompressible, ideal fluid using the vortex contour dynamics technique and the boundary integral equation method. The flow is axisymmetric and the vorticity is linearly distributed in the vortex. Effects of the gravity and the surface tension as well as the initial geometric parameter of the vortex on the interaction process are investigated in considerable detail. The interaction process may be divided into three major stages: the vortex free-traveling stage, the collision stage, and the vortex stretching and rebounding stage. Time evolutions of both the vortex and free surface under various conditions are provided and analyzed. Two kinds of waves exist on the free surface during interaction. In a special case where the gravity and surface tension are very weak or the vortex is very strong, an electric-bulb-like 'cavity' is formed an the free surface and the vortex is trapped in the 'cavity' for quite a. long time, resulting in a large amount, of fluid above the mean fluid surface. 展开更多
关键词 vortex ring vortex dynamics contour dynamics nonlinear free surface
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EVOLUTION OF SINGLE ELLIPTIC VORTEX RINGS
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作者 Zhao, Y Shi, XG 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1997年第1期17-25,共9页
The evolution of single elliptic vortex rings for initial aspect ratio (AR) = 2,4,6 has been studied. The incompressible Navier-Stokes equations are solved by a dealiased pseudo-spectral method with 64(3) grid points ... The evolution of single elliptic vortex rings for initial aspect ratio (AR) = 2,4,6 has been studied. The incompressible Navier-Stokes equations are solved by a dealiased pseudo-spectral method with 64(3) grid points in a periodic cube. We find that there are three kinds of vortex motion as AR increases and bifurcation occurs at certain AR. The processes of advection, interaction and decay of vortex ring are discussed. Numerical results coincide with experiments and other authors' numerical simulation. 展开更多
关键词 elliptic vortex ring pseudo-spectral method BIFURCATION vortex reconnection
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Three-dimensional numerical simulation of a vortex ring impacting a bump
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作者 Heng Ren Changyue Xu 《Theoretical & Applied Mechanics Letters》 CAS 2014年第3期42-48,共7页
A vortex ring impinging on a three-dimensional bump is studied using large eddy simulation for a Reynolds number Re = 4 × 104 based on the initial translation speed and diameter of the vortex ring. The effects of... A vortex ring impinging on a three-dimensional bump is studied using large eddy simulation for a Reynolds number Re = 4 × 104 based on the initial translation speed and diameter of the vortex ring. The effects of bump height on the vortical flow phenomena and the underlying physical mechanisms are inves- tigated. Based on the analysis of the evolution of vortical structures, two typical kinds of vortical structures, i.e., the wrapping vortices and the hair-pin vortices, are identified and play an important role in the flow state evolution. The circu- lation of the primary vortex ring reasonably elucidates some typical phases of flow evolution. Furthermore, the mechanism of flow transition from laminar to turbulent state has been revealed based on analysis of turbulent kinetic energy. 展开更多
关键词 large eddy simulation vortex ring BUMP vortical structure turbulent state
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Effect of pressure evolution on the formation enhancement in dual interacting vortex rings
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作者 Jianing Dong Yang Xiang +1 位作者 Hong Liu Suyang Qin 《Chinese Physics B》 SCIE EI CAS CSCD 2022年第8期470-478,共9页
In the biological locomotion,the ambit pressure is of particular importance to use as a means of propulsion.The multiple vortex rings have been proved to generate additional thrust by interaction,but the mechanism of ... In the biological locomotion,the ambit pressure is of particular importance to use as a means of propulsion.The multiple vortex rings have been proved to generate additional thrust by interaction,but the mechanism of this thrust enhancement is still unknown.This study examines the effect of ambit pressure on formation enhancement in interacting dual vortex rings.The vortex rings,which have the same formation time,are successively generated in a piston-cylinder apparatus.The finite-time Lyapunov exponent(FTLE)visualizes the flow fields as an indication of Lagrangian coherent structures(LCSs),and the pressure field is calculated based on the digital particle image velocity(DPIV).We extract the back pressure of the rear vortex in dual vortices and the back pressure circulationΓ_(b),which is defined as a form of overpressure circulationΓ_(p).TheΓ_(b)has a positive linear relationship withΓ_(p).A critical interval distance d*_(cr)in a range of0.32-0.42 is found whereΓbandΓp reach the maximum synchronously,leading to a full-interaction mode.Moreover,an over-interaction mode and an under-interaction mode are proposed when the dimensionless interval distance d*_(is)smaller or larger than d*_(cr).To conclude,the high back pressure caused by vortex interaction can enhance the formation of vortex rings and lead to high thrust. 展开更多
关键词 vortex ring OVERPRESSURE back pressure finite-time Lyapunov exponent(FTLE)
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A modeling method of microburst based on multiple vortex ring
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作者 林连雷 闫芳 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2012年第6期111-114,共4页
Microburst is a special kind of low-level wind shear, which may do great damage to aircrafts. Modelling of a microburst is significant for flight simulations. In this paper we adopt multiple vortex ring principle to m... Microburst is a special kind of low-level wind shear, which may do great damage to aircrafts. Modelling of a microburst is significant for flight simulations. In this paper we adopt multiple vortex ring principle to model microburst and propose a new parameter selection method of multiple vortex ring model. We treat the parameters selection as an optimization problem, and introduce the differential evolution algorithm into it. A nested differential evolution algorithm is proposed to complete the two optimization process, objective optimization and intermediate optimization. The simulation results show that this method can flexibly generate microburst with any maximum wind velocity. 展开更多
关键词 MICROBURST multiple vortex ring parameter selection nested differential evolution
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Compression and stretching of ring-vortex solitons in a bulk nonlinear medium
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作者 来娴静 蔡晓鸥 张解放 《Chinese Physics B》 SCIE EI CAS CSCD 2015年第7期162-168,共7页
Compression and stretching of ring-vortex solitons, which is a novel self-similar solution of(2+1)-dimensional diffraction decreasing waveguide, is investigated analytically and numerically. We obtain the ring-vort... Compression and stretching of ring-vortex solitons, which is a novel self-similar solution of(2+1)-dimensional diffraction decreasing waveguide, is investigated analytically and numerically. We obtain the ring-vortex solitons via the similarity transformation method. The distance modulation for the width, the diffraction, and the nonlinear response, strongly affects the form and the behavior of the self-similar vortex, and facilitates the efficient compression of optical waves. This approximate ring-vortex solitons can reflect the real properties of self-similar optical vortex beams during propagation under certain parameter window selection. Specific examples and figures are given to illustrate discussed features. The results obtained in this paper may have potential values for all-optical data-processing schemes and the design of beam compressors and amplifiers. 展开更多
关键词 graded-index waveguides ring-vortex soliton INHOMOGENEOUS
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Interaction of Bubbles with Vortex Ring Launched into Bubble Plume
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作者 Tomomi Uchiyama Sou Kusamichi 《Advances in Chemical Engineering and Science》 2013年第4期207-217,共11页
This study is concerned with an experimental exploration for the interactions of bubbles with a vortex ring launched vertically upward into a bubble plume. A vortex ring launcher, composed of a cylinder and a piston, ... This study is concerned with an experimental exploration for the interactions of bubbles with a vortex ring launched vertically upward into a bubble plume. A vortex ring launcher, composed of a cylinder and a piston, is mounted at the bottom of a water tank. Small hydrogen bubbles are released into still water from a cathode, which is wound around the cylinder outlet, by the electrolysis of water. The bubbles rise by the buoyant force and induce a bubble plume. The water in the cylinder is discharged into the bubble plume by the piston, resulting in a laminar vortex ring convecting along the central axis of the plume. Just after the launch of the vortex ring, the bubbles are spirally entrained into the vortex ring with the roll up of the shear layer. The void fraction within the vortex ring increases with the convection of the vortex ring until a certain displacement of the vortex ring, where the reduction occurs. The vortex ring convects with a constant velocity higher than that in still water. The entrained bubbles reduce the strength of the vortex ring. 展开更多
关键词 vortex ring BUBBLE PLUME BUBBLE ENTRAINMENT VORTICITY Visualization PIV
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Quality Assuring a Ring Vortex Flow Phantom in Real-Time
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作者 Alana S. Matthews Kelvin Simatwo +3 位作者 Andrew Narracott Simone Ambrogio Adrian Walker John W. Fenner 《Open Journal of Medical Imaging》 2023年第1期11-29,共19页
Introduction: The ring vortex phantom is a novel, cost-effective prototype which generates complex and well-characterised reference flows in the form of the ring vortex. Although its reproducibility has been demonstra... Introduction: The ring vortex phantom is a novel, cost-effective prototype which generates complex and well-characterised reference flows in the form of the ring vortex. Although its reproducibility has been demonstrated, with ring speeds routinely behaving within 10% tolerances at speeds of approximately 10 - 70 cm/s, a form of real-time QA of the device at the time of imaging is needed to confirm correct function on demand in any environment. Methods: The technology described here achieves real-time QA, comprising a linear encoder, laser-photodiode array, and Doppler probe, measuring piston motion, ring speed and intra-ring velocity respectively. This instrumentation does not interfere with imaging system QA, but allows QA to be performed on both the ring vortex and the device in real-time. Results: The encoder reports the reliability of the piston velocity profile, whilst ring speed is measured by laser behaviour. Incorporation of a calibrated Doppler probe offers a consistency check that confirms behaviour of the central axial flow. For purposes of gold-standard measurement, all elements can be related to previous Laser PIV acquisitions with the same device settings. Conclusion: Consequently, ring vortex production within tolerances is confirmed by this instrumentation, delivering accurate QA in real-time. This implementation offers a phantom QA procedure that exceeds anything seen in the literature, providing the technology to enhance quantitative assessment of flow imaging modalities. 展开更多
关键词 Flow Phantom ring vortex Quality Assurance IMAGING
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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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多毛羽纱线的高品质再造成纱技术及应用
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作者 夏治刚 《纺织高校基础科学学报》 2025年第1期22-24,共3页
短纤纱成形的本质是将散纤维加工成按纵向有序排列的线性集合体。短纤纱成形方法主要有开放端和握持端纺纱^([1])。开放端纺纱以转杯纺、涡流纺为代表,共同点在于:纤维须条在非握持状态下加捻成纱,加捻、卷绕位置分开,实现高速成纱;开... 短纤纱成形的本质是将散纤维加工成按纵向有序排列的线性集合体。短纤纱成形方法主要有开放端和握持端纺纱^([1])。开放端纺纱以转杯纺、涡流纺为代表,共同点在于:纤维须条在非握持状态下加捻成纱,加捻、卷绕位置分开,实现高速成纱;开放端纺纱以纤维缠绕结构为主,其中转杯纺以纤维搭接加捻缠绕方式成形,纱体呈内紧外松式层状包缠结构^([2]);涡流纺以前纤维尾端连续包缠后纤维头端的方式包缠成纱,纱体纤维呈螺旋直径递增的单螺旋包缠结构^([3]),纱表面光洁度、紧密度高,对应织物抗起球等级高。但包缠成纱结构决定了纱体纤维内外转移不足、抱合力差^([4]),纱强低、纱表摩擦易解缠,严重制约纱线高强稳固的高品质成形。 展开更多
关键词 多毛羽纱线 短纤纱 高品质成纱技术 转杯纺 涡流纺 环锭纺
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分布式电推进飞机动力偏航过程滑流效应建模与分析
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作者 田宇 寇鹏 +3 位作者 姚轩宇 郭瑞 梁博华 梁得亮 《航空动力学报》 北大核心 2025年第8期174-186,共13页
在推力差动过程中,不同推进器滑流效应对覆盖区域的升力与阻力影响不同,会产生附加的横侧向力矩,这是动力偏航控制中必须考虑的因素。建立了涡管涡环耦合模型评估分布式电推进器与机翼之间的气动干扰。通过模型计算偏航过程中由螺旋桨... 在推力差动过程中,不同推进器滑流效应对覆盖区域的升力与阻力影响不同,会产生附加的横侧向力矩,这是动力偏航控制中必须考虑的因素。建立了涡管涡环耦合模型评估分布式电推进器与机翼之间的气动干扰。通过模型计算偏航过程中由螺旋桨滑流效应引起的横侧向力矩,完善了考虑滑流效应的分布式电推进飞机横航向飞行动力学方程,并构造了动力偏航控制器。进行动力偏航仿真,从偏航过程中截取一个时刻的飞行状态,将模型计算结果与CFD仿真结果进行对比。对比结果显示,涡管涡环耦合模型可有效刻画分布式电推进飞机偏航过程中滑流效应对机翼的气动影响,其中,由滑流效应产生滚转力矩的计算误差为3.22%,耗时小于5 min。 展开更多
关键词 分布式电推进 横航向 推力差动 滑流效应 涡管涡环耦合模型
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垂直下降状态下螺旋桨气动特性及涡环特征
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作者 高泽明 邵雪明 +2 位作者 王家鼎 曾丽芳 黎军 《空气动力学学报》 北大核心 2025年第1期1-11,I0001,共12页
螺旋桨在垂直下降状态下极易进入涡环状态,从而引起复杂的空气动力学特性。采用黏性涡粒子方法(viscous vortex particle method,VVPM),对APC thin electric 10X7螺旋桨在不同垂直下降率下的气动特性和涡环特征开展研究。结果表明:螺旋... 螺旋桨在垂直下降状态下极易进入涡环状态,从而引起复杂的空气动力学特性。采用黏性涡粒子方法(viscous vortex particle method,VVPM),对APC thin electric 10X7螺旋桨在不同垂直下降率下的气动特性和涡环特征开展研究。结果表明:螺旋桨气动特性容易受到下降率的影响,当下降率增加时,拉力呈现先略增大再减小后增大的趋势,同时尾迹压缩效应逐渐增强,涡环中心逐渐上移。在此过程中,涡环先后经历了悬停状态、涡环前期、涡环初期、深度涡环和类风车流动状态,涡环特征从管状螺旋下洗涡逐渐演变成螺旋涡与环形涡并存,再到完全涡环结构,最后涡系结构移动至桨盘上方。涡场拓扑结构的演变直接影响螺旋桨的气动特性,当桨盘附近尾迹为管状螺旋涡结构时,螺旋桨气动特性变化不明显;随着下降率的增加,逐渐演变出的环形涡会严重影响螺旋桨的气动特性,表现为拉力骤降,尾迹压缩效应增强,回流区包裹桨盘;随着下降率进一步增加,涡系结构到达桨盘上方,螺旋桨进入类风车状态,气动力逐渐增大。 展开更多
关键词 涡环状态 螺旋桨 黏性涡粒子 气动特性 涡环特征
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适用于飞行力学分析的旋翼涡环状态入流模型
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作者 文镜涵 吉洪蕾 +1 位作者 邓皓轩 王畅 《航空学报》 北大核心 2025年第12期132-144,共13页
面向直升机特情仿真的应用需求,建立适用于飞行力学分析的旋翼涡环状态入流模型。基于旋翼涡环状态直升机垂向运动阻尼的转折关系,联立桨尖涡运动方程和修正旋翼动量理论方程来求解旋翼涡环状态临界阻尼边界,获得旋翼进入和改出涡环状... 面向直升机特情仿真的应用需求,建立适用于飞行力学分析的旋翼涡环状态入流模型。基于旋翼涡环状态直升机垂向运动阻尼的转折关系,联立桨尖涡运动方程和修正旋翼动量理论方程来求解旋翼涡环状态临界阻尼边界,获得旋翼进入和改出涡环状态的爬升速度和旋翼诱导速度,采用三次样条函数建立旋翼涡环状态诱导速度模型,并由涡环状态集中涡量的演化关系推导出旋翼涡环状态诱导速度动态延迟时间常数,形成统一的旋翼涡环状态临界阻尼边界和动态入流模型。在此基础上,建立旋翼气动载荷模型和直升机涡环状态的飞行动力学模型,综合采用风洞和飞行试验数据来验证模型。结果表明:所提模型能够合理准确地预测旋翼涡环状态临界阻尼边界及旋翼诱导速度随直升机下降速度和前飞速度的变化,与旋翼气动载荷模型结合能够准确预测旋翼拉力和扭矩系数增量随直升机下降速度的变化趋势;与飞行试验数据的对比表明,所提模型准确模拟了旋翼涡环状态的直升机垂向阻尼动态特性,适用于飞行力学分析应用。 展开更多
关键词 直升机 旋翼 涡环状态 诱导速度 飞行力学
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旋翼间气动干扰对四旋翼飞行器涡环状态影响研究
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作者 李垠翰 苏大成 +2 位作者 杨仁国 吴令华 黄水林 《西北工业大学学报》 北大核心 2025年第5期853-861,共9页
为探究多旋翼之间气动干扰对涡环特性的影响及内在机理,运用分离涡模拟(DES)与嵌套网格相结合的方法,对涡环状态下四旋翼飞行器非定常气动载荷变化特征进行了模拟研究。结果表明:对于文中使用的四旋翼飞行器,在涡环状态前期,由于旋翼间... 为探究多旋翼之间气动干扰对涡环特性的影响及内在机理,运用分离涡模拟(DES)与嵌套网格相结合的方法,对涡环状态下四旋翼飞行器非定常气动载荷变化特征进行了模拟研究。结果表明:对于文中使用的四旋翼飞行器,在涡环状态前期,由于旋翼间的气动干扰,形成了覆盖整个桨盘的大尺度环流结构,旋翼拉力较孤立旋翼的时均值增加17%,非定常波动幅度减少28%,旋翼间气动干扰缓解了涡环状态的不利影响。进入中期,环流结构向上偏移并趋于对称,气动干扰的积极作用有所减弱,但仍使旋翼拉力较孤立旋翼增加11%,非定常波动幅度减少21%。发展至后期,桨盘上方环流现象消失,拉力较孤立旋翼增加27%,非定常波动幅度减少40%,旋翼间干扰效应加速飞行器摆脱涡环环流。旋翼间的气动干扰在涡环状态的不同阶段均对四旋翼飞行器的性能产生了重要影响,尤其在后期阶段表现出显著的积极作用。 展开更多
关键词 涡环状态 四旋翼飞行器 气动干扰 分离涡模拟
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空气辅助喷射系统喷雾过程与雾化机制的数值模拟
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作者 邱豪佶 黄云龙 +1 位作者 何志霞 钟汶君 《内燃机工程》 北大核心 2025年第3期27-38,共12页
为深入研究空气辅助喷射系统内外喷雾过程及气液相互作用引起的雾化机制,基于欧拉–拉格朗日法建立了包括完整空气辅助喷油器和定容环境体的数值模型,并提出了更精确且通用的喷雾模型设置。喷雾过程分为油气混合阶段和混合物喷射阶段。... 为深入研究空气辅助喷射系统内外喷雾过程及气液相互作用引起的雾化机制,基于欧拉–拉格朗日法建立了包括完整空气辅助喷油器和定容环境体的数值模型,并提出了更精确且通用的喷雾模型设置。喷雾过程分为油气混合阶段和混合物喷射阶段。研究定性分析了油气混合阶段中燃油射流的表面破碎过程及液滴与壁面的反弹、飞溅和黏滞行为,明确混合腔设计在气液混合效率与进气稳定性中的关键作用。混合物喷射阶段的结果表明,定容环境体内液滴平均直径约为6μm,拉瓦尔喷嘴出口处存在部分平均直径为20~30μm的液滴。此外,进一步的雾化机制研究发现,出口区域还存在少量平均直径大于50μm的液滴,且这些液滴来源于外壁面上油膜的分离。研究还揭示了涡环的形成机制:近场涡环由拉瓦尔喷嘴的几何形状决定,而远场涡环则由高速空气通过黏性力扰动静止环境氮气产生。最后,通过对空气辅助喷油器各壁面油膜质量变化的分析发现,上内壁面存在大量难以剥离的油膜,这可能导致冷起动过程中燃油积聚问题。 展开更多
关键词 空气辅助喷射系统 欧拉–拉格朗日法 油膜分离与剥离 涡环 油膜质量
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