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Visualization of the Precessing Vortex Core in a Cyclone Separator by PIV 被引量:8
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作者 吴小林 时铭显 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2003年第6期633-637,共5页
The precessing vortex core (PVC) in a cyclone separator plays an important role in the separation performance and in further understanding of the general law of periodic unsteady flow therein. In this paper, the unste... The precessing vortex core (PVC) in a cyclone separator plays an important role in the separation performance and in further understanding of the general law of periodic unsteady flow therein. In this paper, the unsteady flow field is investigated with particle image velocimetry (PIV), and the instantaneous velocity, vorticity, tangential velocity, and radial velocity are acquired by analyzing the images of instantaneous flow. It is for the first time reported that there is a centrifugal flow region close to the dust discharge zone and its maximum value is higher than the mean radial velocity. This discovery is very important for understanding the principle of separation of particles in the area of dust discharge. Determination of the frequency and amplitude of PVC was conducted in the region where the phenomenon of PVC is remarkable. Results agree well with those obtained by hot wire anemometry. The observations of the center of vortex core and the bimodal distribution of the amplitude of the PVC indicate the vortex core precesses around the geometric axis of the cyclone in its own way. 展开更多
关键词 cyclone separator flow field instantaneous velocity precessing vortex core particle image velocimetry
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Analysis of the nutation and precession of the vortex core and the influence of operating parameters in a cyclone separator 被引量:2
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作者 Pan Zhang Guanghui Chen +2 位作者 Weiwen Wang Guodong Zhang Huaming Wang 《Chinese Journal of Chemical Engineering》 SCIE EI CAS CSCD 2022年第6期1-10,共10页
Vortices motion in the anisotropic turbulent flow of cyclones makes a vital impact on flow stability and collection performance.Nevertheless,there remains a lack of clarity in the overall feature of vortices motion.In... Vortices motion in the anisotropic turbulent flow of cyclones makes a vital impact on flow stability and collection performance.Nevertheless,there remains a lack of clarity in the overall feature of vortices motion.In this work,a numerical analysis was conducted to clarify the complex motion of the vortex core in a cyclone separator.The validity of the numerical model was demonstrated by comparing the computational results with experimental data in the literature.As revealed by the results,the vortex core not only has a precession motion about the geometrical center axis but also does a nutation motion in the axial direction.The frequencies of the precession motions show two main peaks.And the magnitudes of the precession and nutation motions have non-uniform distributions in the cyclone.Moreover,the precession-nutation motions of the vortex cores exhibit a similar fluctuant pattern to the dust ring on the separator wall.The inlet gas velocity and the inlet solid loading show vital effects on the magnitudes and frequencies of precession and nutation motion. 展开更多
关键词 Cyclone separator Precession vortex core Nutation motion Separation efficiency Numerical simulation Fluid mechanics
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Faster vortex core switching with lower current density using three-nanocontact spin-polarized currents in a confined structure
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作者 Hua-Nan Li Zhong Hua Dong-Fei Li 《Chinese Physics B》 SCIE EI CAS CSCD 2017年第1期449-453,共5页
We perform micromagnetic simulations on the switching of magnetic vortex core by using spin-polarized currents through a three-nanocontact geometry. Our simulation results show that the current combination with an app... We perform micromagnetic simulations on the switching of magnetic vortex core by using spin-polarized currents through a three-nanocontact geometry. Our simulation results show that the current combination with an appropriate current flow direction destroys the symmetry of the total effective energy of the system so that the vortex core can be easier to excite,resulting in less critical current density and a faster switching process. Besides its fundamental significance, our findings provide an additional route to incorporating magnetic vortex phenomena into data storage devices. 展开更多
关键词 magnetic vortex core polarity switching spin-polarized current micromagnetic simulations
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Prediction of the precessing vortex core in the Francis-99 draft tube under off-design conditions by using Liutex/Rortex method 被引量:6
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作者 Cong Trieu Tran Xin-ping Long +1 位作者 Bin Ji Chaoqun Liu 《Journal of Hydrodynamics》 SCIE EI CSCD 2020年第3期623-628,共6页
The turbulent flow in the draft tube of a Francis turbine is very complicated while working under off-design conditions. Although the off-design conditions were widely studied, the vortex core line in the draft tube o... The turbulent flow in the draft tube of a Francis turbine is very complicated while working under off-design conditions. Although the off-design conditions were widely studied, the vortex core line in the draft tube of a Francis turbine with splitter blades is not well understood, especially the vortex rope property. This letter presents a prediction of the behavior of the vortex rope in the draft tube of the Francis-99 turbine obtained by the computational fluid dynamics (CFD), where the Liutex/Rortex method, as the most recent vortex definition, is applied to analyze the periodical precession of the vortex rope in the draft tube cone. The advantage of this Liutex/Rortex method is shown by its enhanced ability to represent the vortex rope structurewith the vortex-core lines. Furthermore, since it seems to be very hard to define a sharp boundary surface for the whole vortex structure, it is advantageousfocusing only on the vortex core line,by which different vortex structures can be clearly differentiated. The evolution of the vortex core and the process of the vortex breakdown in the draft tube are revealed, which might help to comprehend the development of the turbulent flow in the draft tube. 展开更多
关键词 Cavitating vortex rope Francis turbine Liutex/Rortex method off-design condition vortex core line
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Numerical analysis of vortex core phenomenon during draining from cylinder tank for various initial swirling speeds and various tank and drain port sizes 被引量:2
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作者 SOHN Chang Hyun SON Jong Hyeon PARK Il Seouk 《Journal of Hydrodynamics》 SCIE EI CSCD 2013年第2期183-195,共13页
A dimple appears on a free surface while rotating a cylinder tank filled with liquid. The dimple starts to concentrically deeper to a drain port at the bottom center of the tank. Over time, the dimple penetrates the d... A dimple appears on a free surface while rotating a cylinder tank filled with liquid. The dimple starts to concentrically deeper to a drain port at the bottom center of the tank. Over time, the dimple penetrates the drain port, a free surface forms a long and slender string shape in the tank, and a so-called vortexing (air core) phenomenon occurs. The generation of a vortex core depends on the size of the tank and drain port, and on the properties of the liquid in the tank. In this study, the liquid level and the time at which the vortex core is initially generated are numerically investigated using different values of tank diameter, drain port diameter, and ini- tial tank rotational speeds. Instead of a full three-dimensional analysis, a two-dimensional axisymmetric simulation is conducted. The momentum conservation equation in the circumferential direction is additionally solved in the two-dimensional mesh system. Several non-dimensional variables are created: the ratio of the air core generation distance and tank diameter, the diameter ratio of the tank and drain port, the rotational Reynolds number, the rotational Froude number, and the rotational Weber number. Finally, the non-dimensional air core generation distance is correlated with the other non-dimensional parameters. 展开更多
关键词 air core vortex core dip penetration vortexing draining
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Novel control method of vortex breakdown over delta wing using dual synthetic jets
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作者 Hao WANG Zhenbing LUO +3 位作者 Xiong DENG Yan ZHOU Zhijie ZHAO Jianyuan ZHANG 《Chinese Journal of Aeronautics》 2025年第5期52-64,共13页
To delay the vortex breakdown position of the slender delta wing,this study innovativelyproposes the application of control near the Leading-Edge Vortex(LEV)core sweeping path,whichis called Coupled Core Rotation Dual... To delay the vortex breakdown position of the slender delta wing,this study innovativelyproposes the application of control near the Leading-Edge Vortex(LEV)core sweeping path,whichis called Coupled Core Rotation Dual Synthetic Jets(CCR-DSJ)control.The results show that thevortex breakdown points at each angle of attack are moved backward after control,and the max-imum delayed displacement is 32.4%of the root chord at 30°.Besides,there is a linear relationshipbetween the breakdown position and the angle of attack after control,indicating that CCR-DSJcontrol has a significant effect on the pressure gradient of the vortex axis.Furthermore,the lift coef-ficient C_(L)is enhanced after control,with a maximum CLincrement of 0.078 at 27°,and an effectiveincrement interval of[25°,32°].This interval is different from most previous studies,which isdirectly related to the position of the actuators.According to the lift change mechanism,the anglesof attack are divided into three stages:Stage 1(a=15°–25°),Stage 2(a=25°–32°),and Stage 3(a=32°–40°).In conclusion,CCR-DSJ control can significantly change the pressure distribution,thereby offering promising prospects for the flight stage of the slender delta wing. 展开更多
关键词 vortex breakdown Delta wing vortex core core rotation Dual synthetic jets
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On the Dynamics of Vortex Filaments and Their Core Structure
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作者 Ting Lu (Courant Institute of Mathematical Sciences, New York University) 《Advances in Manufacturing》 SCIE CAS 1999年第2期3-10,共8页
We give a brief review of the asymptotic theory of slender vortex filaments with emphases on (i) the choices of scalings and small parameters characterizing the physical problem,(ii) the key steps in the formulation o... We give a brief review of the asymptotic theory of slender vortex filaments with emphases on (i) the choices of scalings and small parameters characterizing the physical problem,(ii) the key steps in the formulation of the theory and (iii) the assumptions and/or restrictions on the theory of Callegari and Ting (1978).We present highlights of an extension of the 1978 asymptotic theory:the analyses for core structures with axial variation.Making use of the physical insights gained from the analyses,we present a new derivation of the evolution equations for the core structure.The new one is simpler and straightforward and shows the physics clearly. 展开更多
关键词 vortex filaments core structure dynamics asymptotic theory
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基于激光雷达的飞机尾涡反演方法改进研究
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作者 魏志强 杨宪康 《激光与红外》 北大核心 2026年第2期211-219,共9页
针对激光雷达径向分辨率偏大、致使尾涡反演精度偏低的问题。通过三次插值和三次样条插值在激光雷达距离门之间按照密度1、2、4、8 m对尾涡径向风场进行插值,并使用梯度法反演涡核位置;然后对梯度法进行改进,在各个距离门的梯度绝对值... 针对激光雷达径向分辨率偏大、致使尾涡反演精度偏低的问题。通过三次插值和三次样条插值在激光雷达距离门之间按照密度1、2、4、8 m对尾涡径向风场进行插值,并使用梯度法反演涡核位置;然后对梯度法进行改进,在各个距离门的梯度绝对值最大值之间使用三次插值和三次样条插值按照密度1、2、4、8 m进行插值。最后提出了基于三次样条插值的分辨率提升方法,通过改进梯度法提高了涡核识别准确度。研究表明,三次样条插值较三次插值对尾涡数据吻合程度更高;在算例中,三次插值涡核位置最高修正率为20%~35%,三次样条插值涡核位置最高修正率为39%~71%;比较尾涡径向风场插值算法和改进梯度法识别涡核的效率,改进梯度法较尾涡径向风场插值算法所用时间提高了82%。 展开更多
关键词 尾涡参数反演 涡核位置估算 激光雷达 飞机尾流 尾涡流场仿真
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竹浆纤维喷气涡流纺夏季用机织物的设计及性能评价
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作者 张会青 高中慧 姚瑞盼 《毛纺科技》 北大核心 2026年第3期11-18,共8页
为了探讨竹浆纤维喷气涡流纺包芯纱在夏季用机织物中的适用性,以竹浆纤维喷气涡流纺包芯纱为原料,通过设计不同纱线类型、芯丝成分与织物组织的多组竹浆纤维夏季用机织物,测试其保形性、透通性及接触凉感等服用性能指标,并基于测试数据... 为了探讨竹浆纤维喷气涡流纺包芯纱在夏季用机织物中的适用性,以竹浆纤维喷气涡流纺包芯纱为原料,通过设计不同纱线类型、芯丝成分与织物组织的多组竹浆纤维夏季用机织物,测试其保形性、透通性及接触凉感等服用性能指标,并基于测试数据运用灰色关联度分析法进行综合评价。结果表明,纺纱方式和芯丝选择、织物组织对竹浆纤维织物的保形性和透通性等服用性能有着不同程度的影响,喷气涡流纺包芯纱独特的成纱机制有效提升了织物的抗弯刚度和抗皱性,吸湿排汗涤纶芯丝则通过毛细效应改善了织物的吸湿快干性能;竹浆纤维喷气涡流纺包芯纱机织物在抗皱性、透气性和透湿性等服用性能方面表现良好,具有一定的接触凉感,适用于夏季衬衫、裙装及家纺产品开发,为竹浆纤维织物的设计与应用提供了理论依据和实践参考。 展开更多
关键词 竹浆纤维 机织物 喷气涡流纺 包芯纱 灰色关联度分析 服用性能
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Trajectory and frequency of vortex gyration in a multi-nanocontact geometry
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作者 李化南 柳艳 +1 位作者 贾敏 杜安 《Chinese Physics B》 SCIE EI CAS CSCD 2015年第4期431-435,共5页
Nonlinear vortex gyrotropic motion in a three-nanocontacts system is investigated by micromagnetic slmulations and analytical calculations. Three out-of-plane spin-polarized currents are injected into a nanodisk throu... Nonlinear vortex gyrotropic motion in a three-nanocontacts system is investigated by micromagnetic slmulations and analytical calculations. Three out-of-plane spin-polarized currents are injected into a nanodisk through a centered nanocontact and two off-centered nanocontacts, respectively. For current combination (ipl, ip0, ip2) = (-1,1, -1), the trajectory of the vortex core is a peanut-like orbit, but it is an elliptical orbit for (ip1, ip0, ip2) = (1, 1, -1). Moreover, the gyrotropic frequency displays peaks for both current combinations. Analytical calculations based on the Thiele equation show that the changes of frequency can be ascribed mainly to the forces generated by the Oersted field accompanying the currents. We also demonstrate a dependence of eigenfrequency shifts on the direction and distance of the applied currents. 展开更多
关键词 vortex core spin-polarized current Oersted field Thiele's equation
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同轴涡环相互作用过程的噪声分析
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作者 臧振宇 周志腾 王士召 《力学进展》 北大核心 2026年第1期260-274,共15页
涡环同轴相互作用是亚音速射流中的典型流动结构和重要的噪声来源.调控涡环相互作用过程的加减速运动是降低射流噪声的关键.已有的研究工作发现,弱涡环径向加速度是低频高振幅噪声的主导因素.本文基于Dyson薄核涡环模型研究了这一现象... 涡环同轴相互作用是亚音速射流中的典型流动结构和重要的噪声来源.调控涡环相互作用过程的加减速运动是降低射流噪声的关键.已有的研究工作发现,弱涡环径向加速度是低频高振幅噪声的主导因素.本文基于Dyson薄核涡环模型研究了这一现象的成立条件和规律.通过将声源分解为涡环轴向和径向动力学参数乘积的形式,研究了不同初始环量比和初始半径比条件下的涡环相互作用过程,发现了主导总声源脉冲的临界初始半径比.只有当初始涡环半径比小于临界初始半径比时,弱涡环径向加速度声源项对总声源的贡献才大于强涡环.通过对涡环相互作用过程的定量分析,发现了声源脉冲峰值与涡环轴向速度、径向加速度峰值的关联关系,并发现强涡环的反向运动,会造成强涡环声源项产生反相位脉冲. 展开更多
关键词 涡环 同轴相互作用 声源 薄核涡环模型 径向加速度
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热带气旋生成前初始中、低层型涡旋的热力结构发展差异
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作者 刘乐 刘岩 唐晓东 《南京大学学报(自然科学版)》 北大核心 2026年第2期204-217,共14页
利用两个实际典型个例分析了热带气旋(TC)生成过程中初始中层(MV)型和低层(LV)型涡旋的发展及作用差异. MV型TC Koinu前期存在持续正温度异常,而LV型TC Mawar中未出现,且Koinu中暖核的出现比Mawar早.由于Mawar中初始暖核高度比Koinu低,... 利用两个实际典型个例分析了热带气旋(TC)生成过程中初始中层(MV)型和低层(LV)型涡旋的发展及作用差异. MV型TC Koinu前期存在持续正温度异常,而LV型TC Mawar中未出现,且Koinu中暖核的出现比Mawar早.由于Mawar中初始暖核高度比Koinu低,当暖核同等增强时,Mawar中低层风增强更快,因此海平面气压径向梯度也增强,产生更强的低层径向流入,更有利于强度增强;同时,Koinu初期中层的冷异常也会抑制其强度增强. Mawar暖核的出现与下沉增暖过程密切相关,而此过程在Koinu中未出现,因此Mawar和Koinu的暖核初始高度不同,最终导致LV型的TC生成效率(以暖核出现作为起始的定义)高于MV型.此外,Koinu和Mawar的暖核出现均早于TC明显增强和达到热带风暴强度,也说明暖核是TC生成的先决条件. 展开更多
关键词 热带气旋 暖核 初始涡旋 生成效率
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喷气涡流纺莱赛尔粘胶锦纶PBT包芯纱的生产
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作者 陈路 汤龙世 +2 位作者 张仕成 徐庆红 李长红 《棉纺织技术》 2026年第1期76-78,共3页
探讨喷气涡流纺莱赛尔粘胶锦纶PBT包芯纱的纺纱技术。针对莱赛尔纤维、粘胶纤维、锦纶的性能特点,为提高其可纺性,在抓包机运行过程中将配制的养生剂均匀喷洒在三组分混纺纤维棉层中;清棉工序使用短流程配置;梳棉工序重点优化锡林刺辊... 探讨喷气涡流纺莱赛尔粘胶锦纶PBT包芯纱的纺纱技术。针对莱赛尔纤维、粘胶纤维、锦纶的性能特点,为提高其可纺性,在抓包机运行过程中将配制的养生剂均匀喷洒在三组分混纺纤维棉层中;清棉工序使用短流程配置;梳棉工序重点优化锡林刺辊线速比;并条工序采用三道并条混和,并优化后区牵伸配置;喷气涡流纺工序优选关键纺纱专件和工艺参数,加严清纱参数设置等措施,最终生产出质量符合使用要求的喷气涡流纺包芯纱。认为:通过优化工艺配置可有效解决喷气涡流纺包芯纱手感偏硬、易产生弱捻纱、包芯纱易露丝等问题,保证了喷气涡流纺包芯纱的质量稳定。 展开更多
关键词 喷气涡流纺 养生剂 莱赛尔纤维 锦纶 PBT长丝 包芯纱
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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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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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逗点状MCS中的γ中尺度涡旋形成机制及结构特征
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作者 徐姝 王艳春 +3 位作者 王莹 庄园煌 易笑园 张文龙 《暴雨灾害》 2025年第5期642-652,共11页
利用自动站观测资料、多普勒天气雷达资料以及ERA5再分析等资料,对2022年7月5日夜间发生在渤海西岸的一次大暴雨过程进行观测和数值预报结果分析,初步探讨了逗点状中尺度对流系统(MCS)中的γ中尺度涡旋形成机制及其结构特征。结果表明:... 利用自动站观测资料、多普勒天气雷达资料以及ERA5再分析等资料,对2022年7月5日夜间发生在渤海西岸的一次大暴雨过程进行观测和数值预报结果分析,初步探讨了逗点状中尺度对流系统(MCS)中的γ中尺度涡旋形成机制及其结构特征。结果表明:暴雨过程发生在高空低槽东移和台风“暹芭”减弱后低压倒槽北抬的天气背景下,由逗点状中尺度对流系统头部的低质心涡旋回波有组织性地持续影响渤海西岸造成。γ中尺度涡旋最初发生在低压倒槽顶部,是由前期降水形成的西北气流和暖湿东南气流相遇后的锋生作用所致,其随后在925 hPa、850 hPa依次出现,降水主要出现在涡旋的右侧。涡度方程的收支诊断表明,涡旋主要由低层水平辐合辐散项提供初始扰动,后通过垂直涡度依次向上输送,最终在对流层下半部形成深厚的中尺度涡旋。涡旋在700—850 hPa附近存在暖心结构,925 hPa以下弱冷空气的渗透为对流雨带的发展提供了热力不稳定和动力强迫作用;涡旋呈现不对称结构特征,其东侧上升速度大于西侧,使得东侧降水明显强于西侧。涡旋的水汽输送也呈明显的不对称结构,水汽辐合主要集中在涡旋东侧即渤海西岸,这也是涡旋东侧降水偏强的原因。 展开更多
关键词 γ中尺度涡旋 锋生 不对称结构 暖心 涡度收支
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低熔点涤纶长丝在高保形针织面料中的应用
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作者 王怡怡 杜立新 +2 位作者 田明伟 曲志强 贾云辉 《服装学报》 北大核心 2025年第4期283-288,共6页
针对针织面料保形性较差的问题,采用涡流纺棉包芯低熔点涤纶长丝纱线(简称低熔点涤纶包芯纱)开发针织面料。通过对比皮芯结构和点状结构两种低熔点涤纶长丝在不同热处理温度下的熔融效果,从水洗尺寸稳定性、折皱回复性、拉伸回复性及抗... 针对针织面料保形性较差的问题,采用涡流纺棉包芯低熔点涤纶长丝纱线(简称低熔点涤纶包芯纱)开发针织面料。通过对比皮芯结构和点状结构两种低熔点涤纶长丝在不同热处理温度下的熔融效果,从水洗尺寸稳定性、折皱回复性、拉伸回复性及抗弯刚度4个方面对针织面料的性能进行系统分析。结果显示,使用低熔点涤纶包芯纱可显著改善面料的水洗尺寸稳定性、折皱回复角和拉伸回复性;随着热处理温度的升高,低熔点涤纶熔融效果越来越显著,面料的保形性进一步提升,但手感变硬。研究表明,皮芯结构低熔点涤纶包芯纱所织面料的保形性优于点状结构低熔点涤纶包芯纱所织面料,但手感更差;皮芯结构低熔点涤纶包芯纱所织面料宜用185℃进行热处理,而点状结构低熔点涤纶包芯纱所织面料宜用195℃进行热处理,以达到针织面料保形性与手感的平衡。 展开更多
关键词 针织面料 涡流纺包芯纱 低熔点涤纶长丝 热处理 高保形
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张力对喷气涡流纺粘胶/锦纶/涤纶长丝包芯纱包覆效果和性能的影响 被引量:2
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作者 杨宇 吴俊年 +2 位作者 龚正晖 傅佳佳 卢雨正 《现代纺织技术》 北大核心 2025年第8期26-34,共9页
为生产包覆效果和成纱性能优良的喷气涡流纺包芯纱,以粘胶和锦纶混合短纤维为外包纤维,涤纶全拉伸丝为芯丝,制备了17.2 tex喷气涡流纺粘胶/锦纶/涤纶长丝包芯纱。使用单因素分析的方法研究了芯丝预加张力和喂入比对张力的影响规律,并在... 为生产包覆效果和成纱性能优良的喷气涡流纺包芯纱,以粘胶和锦纶混合短纤维为外包纤维,涤纶全拉伸丝为芯丝,制备了17.2 tex喷气涡流纺粘胶/锦纶/涤纶长丝包芯纱。使用单因素分析的方法研究了芯丝预加张力和喂入比对张力的影响规律,并在此基础上研究了张力对喷气涡流纺包芯纱成纱结构、包覆效果和成纱性能的影响,最终提取最优成纱工艺。结果表明:芯丝预加张力和喂入比都影响包覆效果和成纱质量,芯丝预加张力2.1 cN和喂入比0.98时,纱线结构最稳定,包覆效果和成纱性能最好。相较于同规格喷气涡流纺粘胶/锦纶混纺纱,工艺优化后的纱线断裂强度提高了24.8%,断裂伸长率提高了9%,弹性回复率提高了9.3%,条干均匀度和毛羽也有所改善。 展开更多
关键词 喷气涡流纺 包芯纱 纺纱段张力 覆盖系数 纱线性能
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低旋流中心分级燃烧室流场特性的超大涡模拟
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作者 葛修良 尚守堂 +2 位作者 胡文成 林宏军 韩省思 《航空发动机》 北大核心 2025年第5期57-63,共7页
为了研究低旋流中心分级燃烧室流场特性,采用超大涡模拟和粒子成像测速(PIV)试验结合的方法,对副模单独工作及不同主副模组合方案开展了研究。结果表明:中心分级燃烧室流场中的进动涡核(PVC)是由副模气流产生的。当副模单独工作时,PVC... 为了研究低旋流中心分级燃烧室流场特性,采用超大涡模拟和粒子成像测速(PIV)试验结合的方法,对副模单独工作及不同主副模组合方案开展了研究。结果表明:中心分级燃烧室流场中的进动涡核(PVC)是由副模气流产生的。当副模单独工作时,PVC改变了流场的结构,涡核破碎导致了流场的非对称现象。当主副模旋流器共同工作时,PVC形成了中心回流区头部区域,由于其进动导致了回流区头部的不稳定现象,在旋流强度低的情况下无法形成连续回流区;主副模气流共同作用形成了中心回流区下游区域,主模进气量对中心回流区下游区域的径向宽度起主要作用,进气量增大会减小中心回流区下游区域的径向宽度。基于功率谱密度识别了PVC的进动频率,相同副模对应的PVC特征频率接近,主模进气流量对PVC特征频率有影响,但无明显规律。 展开更多
关键词 燃烧室 旋流 中心分级 超大涡模拟 进动涡核 航空发动机
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加油机近场尾涡影响规律及危险区域评估
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作者 王玉琰 刘峰博 +2 位作者 张文豪 肖峰 梁益华 《西北工业大学学报》 北大核心 2025年第3期564-573,共10页
加油机尾涡的发展包括近场和远场2个阶段,近场阶段尾涡处于卷起和成熟期,尾涡的演化机理复杂且形成的尾涡强度较大,对下游飞机特别是中小型无人受油机的安全性和稳定性会造成不利影响,因此需要重点研究近场尾涡的发展及影响规律,通过分... 加油机尾涡的发展包括近场和远场2个阶段,近场阶段尾涡处于卷起和成熟期,尾涡的演化机理复杂且形成的尾涡强度较大,对下游飞机特别是中小型无人受油机的安全性和稳定性会造成不利影响,因此需要重点研究近场尾涡的发展及影响规律,通过分析尾涡流场对其潜在的危险区域进行评估。采用雷诺平均方法模拟以CRM飞机为假想加油机的尾涡的近场分布,对不同来流马赫数和侧风条件下加油机近场尾涡的涡核位置和影响规律及范围进行分析,在此基础上以“捕食者”无人机构型为受油机研究对象,选取临界滚转力矩系数作为危险区域判据,通过计算分析评估了受油机在CRM加油机后的尾涡危险区域。研究结果表明,增大马赫数使得涡核在下落阶段纵向位置更低,涡核半径变大,尾涡环量变大;侧风使涡核位置出现明显偏移,侧风越大,偏移量越大,同时会加速尾涡耗散;在加油机尾涡流场影响下,受油机面临的潜在危险区域主要受加油机尾涡环量和受油机特征参数影响,且危险区域位置与涡核位置变化保持一致。 展开更多
关键词 近场尾涡 尾涡发展规律 涡核位置 尾涡耗散 危险区域
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