期刊文献+
共找到44篇文章
< 1 2 3 >
每页显示 20 50 100
两种特殊CTS试验技术的研究 被引量:9
1
作者 于志松 王发祥 罗新福 《实验流体力学》 EI CAS CSCD 北大核心 2004年第4期49-53,共5页
介绍了载机投放/发射的外挂武器具有舵面控制律模拟的分离轨迹测量技术以及分离体带喷流的导弹级间分离气动干扰特性测量技术的研究情况。研究表明,两种特殊CTS试验技术研究取得了比较满意的结果,进一步拓展了气动中心1.2m高速风洞捕获... 介绍了载机投放/发射的外挂武器具有舵面控制律模拟的分离轨迹测量技术以及分离体带喷流的导弹级间分离气动干扰特性测量技术的研究情况。研究表明,两种特殊CTS试验技术研究取得了比较满意的结果,进一步拓展了气动中心1.2m高速风洞捕获轨迹综合试验能力和种类。 展开更多
关键词 试验技术 外挂物分离 轨迹特性 气动干扰 喷流
下载PDF
自动消防水炮性能参数对射流轨迹的影响 被引量:7
2
作者 刘正勤 《消防科学与技术》 CAS 北大核心 2015年第11期1471-1474,共4页
针对影响自动消防炮射流轨迹的几个主要性能参数,如压力、喷嘴流量、俯仰角、安装高度等进行了试验研究,分析各个参数对射流轨迹影响的规律。测试远程喷射过程中的水流轨迹形态,使用MATLAB对测试曲线进行拟合以弥补后台数据的不足。从... 针对影响自动消防炮射流轨迹的几个主要性能参数,如压力、喷嘴流量、俯仰角、安装高度等进行了试验研究,分析各个参数对射流轨迹影响的规律。测试远程喷射过程中的水流轨迹形态,使用MATLAB对测试曲线进行拟合以弥补后台数据的不足。从工程调试的角度对自动消防水炮系统喷射误差的成因进行分析,提出了提高喷射精准度的方案和解决思路。 展开更多
关键词 消防水炮 射流轨迹 喷射误差
下载PDF
Theoretical Analysis of A Buoyant Jet Interacting with Small Amplitude Waves 被引量:5
3
作者 Ying-Pin LIN Hung-Chu HSU Yang-Yih CHEN 《China Ocean Engineering》 SCIE EI 2009年第1期73-84,共12页
A new theoretical solution is presented here for the dynamic characteristics of a buoyant jet due to opposing small amplitude waves. The conservation equations of mass, tangential moment^n and vertical momentum are so... A new theoretical solution is presented here for the dynamic characteristics of a buoyant jet due to opposing small amplitude waves. The conservation equations of mass, tangential moment^n and vertical momentum are solved by the integral method which encompasses the Gaussian profiles of velocity and density. The action of waves is incorporated into the equations of motion as an external force and a new exact solution is obtained to predict the trajectory, velocity distribution and boundary thickness of the buoyant jet over an arbitrary lateral cross section. It is found that the velocity along the centerline is inversely proportional to the ratio of the momentum of the wave to the buoyant jet. The averaged bound- ary width varies with the fluctuation of the boundary width, the distance from the orifice and the velocity correction function. Owing to the motion of waves, the fluctuation of the boundary width is proportional to the wave steepness. 展开更多
关键词 buoyant jet small amplitude waves radiation stress jet trajectory
下载PDF
消防水炮水力学性能研究综述 被引量:5
4
作者 袁晓明 王超 +1 位作者 赵斌 杨庆祥 《机械设计》 CSCD 北大核心 2017年第1期1-8,共8页
介绍了消防水炮的结构形式,对与消防水炮水力学性能相关的射流稳定性、结构设计与优化和射流轨迹3部分内容进行了分析。总结了目前消防水炮研究过程中存在的局限性,并对未来消防水炮的发展进行了展望。
关键词 消防水炮 水力学性能 射流稳定性 射流轨迹
下载PDF
Ski jump trajectory with consideration of air resistance 被引量:4
5
作者 吴建华 张晓艳 +1 位作者 马飞 吴伟伟 《Journal of Hydrodynamics》 SCIE EI CSCD 2015年第3期465-468,共4页
In the case of the ski-jump type energy dissipation, the jet trajectory will be greatly affected by the air entrainment and the air resistance. It is necessary to consider those factors when estimating the trajectory ... In the case of the ski-jump type energy dissipation, the jet trajectory will be greatly affected by the air entrainment and the air resistance. It is necessary to consider those factors when estimating the trajectory of the jet flow. In this work, the effect of the air resistance on the jet trajectory is theoretically and experimentally investigated. A comprehensive resistance coefficient is proposed. To determine this coefficient, experiments of five models are conducted with the circular-shaped flip bucket placed at the point of the takeoff of ski jumps. It is shown that, this coefficient of the lower jet trajectory is only related to the approach flow Froude number, while that of the upper jet trajectory is dominated by both this Froude number and the deflection angle. Furthermore, the present methodology is validated by experimental data in this work and the maximum errors are not larger than 3.2% and 8.6% for the lower and upper jet trajectories, respectively. 展开更多
关键词 trajectory jet flow comprehensive resistance coefficient hydropower project
原文传递
基于OpenFOAM对某溢洪道挑流水动力特性的两相流数值研究
6
作者 刘晗月 任春平 黄旭中 《水电能源科学》 北大核心 2024年第1期115-119,共5页
挑流消能中水舌在空中段及跌落到下游水垫塘的过程中,均存在明显的气液两相流特性,为更加深入探明该过程中的水动力特性,需构建更加先进的气液两相流数值模型。运用CFD开源软件OpenFOAM构建两相流三维数值模型,通过挑流试验测得的水舌... 挑流消能中水舌在空中段及跌落到下游水垫塘的过程中,均存在明显的气液两相流特性,为更加深入探明该过程中的水动力特性,需构建更加先进的气液两相流数值模型。运用CFD开源软件OpenFOAM构建两相流三维数值模型,通过挑流试验测得的水舌结果对该数值模型进行验证,结果表明数值模拟结果与试验结果吻合较好,同时通过数值研究发现κ-ωSST湍流模型优于κ-ε、κ-ω湍流模型。将κ-ωSST湍流模型得到的数值模拟结果与已有挑流射程经验公式进行比较,结果表明κ-ωSST湍流模型比经验公式计算结果更接近试验结果。最后,基于数值模拟结果分析射流作用下水垫塘的动水压力分布特征,发现塘底湍动能最大值位于距挑坎1.26L_(1)、1.23L_(2)、1.093L_(3)、1.001L_(4)处。最大塘底压强位于距挑坎约0.91L3处,此处也是整个计算域流速最低的流速滞点。研究结果可为挑流过程的相关研究提供参考。 展开更多
关键词 挑流 气液两相流 OPENFOAM 模型试验 湍流模型
下载PDF
平底差动坎的流态和水舌挑距 被引量:3
7
作者 孙红娟 马飞 骆超 《水电能源科学》 北大核心 2017年第3期98-100,共3页
为更准确地计算平底差动坎的水舌挑距,对平底差动坎进行了物理模型试验,采用水舌运动轨迹公式估算差动坎水舌挑距,并根据理论分析和模型试验结果,修正了上股水舌挑距估算公式中的出射角及下股水舌挑距估算公式中的出射流速,由此得到了... 为更准确地计算平底差动坎的水舌挑距,对平底差动坎进行了物理模型试验,采用水舌运动轨迹公式估算差动坎水舌挑距,并根据理论分析和模型试验结果,修正了上股水舌挑距估算公式中的出射角及下股水舌挑距估算公式中的出射流速,由此得到了系列差动坎水舌挑距估算公式,其计算值与试验值吻合良好,误差控制在10%以内,可为工程设计提供参考。 展开更多
关键词 平底差动坎 流态 水舌挑距 出射流速 出射角
下载PDF
Hydraulics of crest spillway with large unit discharge and low Froude number 被引量:2
8
作者 吴建华 李程纯子 +2 位作者 马飞 李同春 吴伟伟 《Journal of Hydrodynamics》 SCIE EI CSCD 2015年第2期242-247,共6页
With respect to the crest spillway with large unit discharge and low Froude number, the hydraulics of the slit-type energy dissipater at the outlet should be noticed due to the complicated flow regimes. In the present... With respect to the crest spillway with large unit discharge and low Froude number, the hydraulics of the slit-type energy dissipater at the outlet should be noticed due to the complicated flow regimes. In the present paper, some issues about hydraulic characteristics were experimentally investigated by means of five slit-type outlets and four tetrahedrons, including the flow choking, impact to river banks and jet trajectory. The main findings are as follows. The critical Froude number for the flow choking decreases with increasing outlet width of the slit-type energy dissipater. If the flow Froude number is expressed by the parameters just before this energy dissipater, the tetrahedron placed inside the side wall of the outlet could efficiently avoid the flow impact to the river bank of same side, and compared with the jet trajectory of the slit-type energy dissipater, the outlet with tetrahedron has different trajectory trend, i.e., the distance of the jet trajectory decreases with the increase of the water head due to special form of the outlet tetrahedron. 展开更多
关键词 large unit discharge low Froude number flow choking impact to river bank jet trajectory
原文传递
Flow choking over weir flow slit-type flip buckets 被引量:2
9
作者 马飞 徐准 吴建华 《Journal of Hydrodynamics》 SCIE EI CSCD 2015年第6期907-912,共6页
The flow choking may occur for weir flow slit-type flip buckets trader common operation conditions. An estimation method is developed through introducing a comprehensive coefficient to determine the approach flow Frou... The flow choking may occur for weir flow slit-type flip buckets trader common operation conditions. An estimation method is developed through introducing a comprehensive coefficient to determine the approach flow Froude number for the flow choking to occur in those flip buckets. The error of the present method relative to the experimental data is less than 5%. The results show that, the Froude number for the flow choking to occur is related to the contraction ratio and the contraction angle of the flip buckets. When the flow choking occurs, the upper jet trajectory decreases and the lower one is almost not affected, and the dynamic pressures on the bottom and the sidewalls increase due to the flow profile rising on the flip buckets. 展开更多
关键词 flow choking jet trajectory dynamic pressure slit-type flip bucket weir flow
原文传递
弹道修正弹脉冲发动机作用角度优化研究 被引量:3
10
作者 田再克 杨锁昌 +1 位作者 冯德龙 姚运志 《弹箭与制导学报》 CSCD 北大核心 2014年第2期105-108,共4页
解算脉冲发动机最佳作用角度是脉冲弹道修正技术的一个重要课题。文中基于传统的脉冲发动机控制策略,从理论上分析了脉冲发动机作用角度与剩余落点偏差,针对横纵脉冲修正能力不同造成剩余落点偏差较大的情况,提出了一种以剩余落点偏差... 解算脉冲发动机最佳作用角度是脉冲弹道修正技术的一个重要课题。文中基于传统的脉冲发动机控制策略,从理论上分析了脉冲发动机作用角度与剩余落点偏差,针对横纵脉冲修正能力不同造成剩余落点偏差较大的情况,提出了一种以剩余落点偏差为目标函数的解算脉冲发动机作用角度算法,并通过六自由度弹道仿真验证了该算法的可行性。 展开更多
关键词 导弹 弹道修正 脉冲发动机 作用角度
下载PDF
TRAJECTORY DIAGNOSIS OF AIR PARCELS IN HIGH-AND LOW-LEVEL JETS FOR A HEAVY RAINFALL CASE DURING MEIYU SEASON OF 1991
11
作者 陶祖钰 黄伟 《Acta meteorologica Sinica》 SCIE 1993年第4期486-494,共9页
Trajectory diagnostic methods were used to analyze air parcels of high- and low-level jets during the heavy rainfall of 4-6 July 1991.It is found that air parcels above rainfall area travelled from the entrance of the... Trajectory diagnostic methods were used to analyze air parcels of high- and low-level jets during the heavy rainfall of 4-6 July 1991.It is found that air parcels above rainfall area travelled from the entrance of the high-level jet,passing through the jet center and reached the exit region.Upper tropospheric divergence over rainfall area resulted from decelerative motion of the jet flow.Warm and moist southwest flow converged and ascended ahead of the low-level jet. The decreasing of low-level pressure as a result of high-level divergence that caused the low-level jet became unexpectedly strong. 展开更多
关键词 heavy rainfall trajectory jet
原文传递
On the trajectory of nonturbulent liquid jets in subsonic crossflows at different density ratios
12
作者 Mehdi Jadidi Ali Dolatabadi 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2018年第4期277-283,300,共8页
Numerical simulations using volume of fluid(VOF)method are performed to study the impact of liquid-to-gas density ratio on the trajectory of nonturbulent liquid jets in gaseous crossflows.In this paper,large eddy simu... Numerical simulations using volume of fluid(VOF)method are performed to study the impact of liquid-to-gas density ratio on the trajectory of nonturbulent liquid jets in gaseous crossflows.In this paper,large eddy simulation(LES)turbulence model is coupled with the VOF method to describe the turbulence effects accurately.In addition,dynamic adaptive mesh refinement method with two refinement levels is applied to refine the size of the cells located at gas-liquid interface.Density ratio is changed from 10 to 5000 while other nondimensional numbers are kept constant.Large density ratios are considered in this paper since they are common in many practical applications such as solution precursor/suspension plasma sprays.Our simulations show that the penetration height,especially in the farfield,increases as the density ratio increases.A general correlation for the jet trajectory,which can be used for a wide range of density ratios,is developed based on our simulation results. 展开更多
关键词 Primary BREAKUP Liquid jet Density ratio Gaseous CROSSFLOW SPRAY trajectory
下载PDF
Comparison of Energy Dissipation with and without Aerators
13
作者 聂孟喜 《Tsinghua Science and Technology》 EI CAS 2000年第2期222-225,共4页
Experimental results showed that aerators increase the energy dissipation of the flow in the channel by reducing the velocity coefficient φ in the deflector bucket and the jet trajectory length, by increasing en... Experimental results showed that aerators increase the energy dissipation of the flow in the channel by reducing the velocity coefficient φ in the deflector bucket and the jet trajectory length, by increasing energy dissipation of the jet flow in the air and the diffusion length of the jet falling into the pool and by reducing the energy intensity of the jet falling into the pool. The energy dissipation prevents wash out downstream.When air is not entrained in the water flow, the aerators act as artificial irregularities in the channel. The energy dissipation due to the aerators in the channel without entrained air is greater than when air is entrained in the water flow.Correlations of the experimental data can be used to estimate the energy dissipation effect of the aerators on the outlet structure for the three test cases. 展开更多
关键词 energy dissipation AERATOR DIFFUSION jet trajectory open channel energy intensity
原文传递
Air-vent layouts and water-air flow behaviors of a wide spillway aerator
14
作者 James Yang Penghua Teng Chang Lin 《Theoretical & Applied Mechanics Letters》 CAS CSCD 2019年第2期130-143,共14页
A spillway aerator should guarantee favorable flow conditions in the coupled water-air system even if the aerator is unconventionally wide. Eight air-vent configurations are devised and incorporated into a 35-m wide c... A spillway aerator should guarantee favorable flow conditions in the coupled water-air system even if the aerator is unconventionally wide. Eight air-vent configurations are devised and incorporated into a 35-m wide chute aerator for a generalized study. Computational fluid dynamics(CFD) simulations are performed to explore their effects on water-jet and air-cavity features. The Re-normalisation group(RNG) k-ε turbulence model and the two-fluid model are combined to predict the two-phase flow field. The results demonstrate appreciable influences of the vent layouts on the water-air flow. The air vents stir the air motion and re-distribute the cavity air pressure. Once the vent layout is modified, reciprocal adjustments exist between the jet behavior and air-pressure field in the cavity, thus leading to considerable differences in air-flow rate, jet-trajectory length, vent air-flow distribution across the chute, etc. The large width plays a discernable role in affecting the aerated flow. Telling differences exist between the near-wall region and the central part of the chute. To improve the duct pressure propagation, a gradual augment of the vent area should be assigned towards the chute center. Relative to single-slot vents across the flow, the layouts with segregated vents gain by comparison. A designer should see to it that a vented aerator operates satisfactorily for a given range of flow discharges. 展开更多
关键词 SPILLWAY WIDE AERATOR AIR entrainment Air-vent layout jet trajectory CFD
下载PDF
Flow-Field Analysis of Anti-Kidney Vortex Film Cooling 被引量:1
15
作者 Lars Grf Leonhard Kleiser 《Journal of Thermal Science》 SCIE EI CAS CSCD 2012年第1期66-76,共11页
Film cooling is an important measure to enable an increase of the inlet temperature of a gas turbine and, thereby, to improve its overall efficiency. The coolant is ejected through spanwise rows of holes in the blades... Film cooling is an important measure to enable an increase of the inlet temperature of a gas turbine and, thereby, to improve its overall efficiency. The coolant is ejected through spanwise rows of holes in the blades or endwalls to build up a film shielding the material. The holes often are inclined in the downstream direction and give rise to a kidney vortex. This is a counter-rotating vortex pair, with an upward flow direction between the two vortices, which tends to lift off the surface and to locally feed hot air towards the blade outside the pair. Reversing the rotational sense of the vortices reverses these two drawbacks into advantages. In the considered case, an anti-kidney vortex is generated using two subsequent rows of holes both inclined downstream and yawed spanwise with alternating angles. In a previous study, we performed large-eddy simulations (which focused on the fully turbulent boundary layer) of this anti-kidney vortex film-cooling and compared them to a corresponding physical experiment. The present work analyzes the simulated flow field in detail, beginning in the plenum (inside the blade or endwall) through the holes up to the mixture with the hot boundary layer. To identify the vortical structures found in the mean flow and in the instantaneous flow, we mostly use the λ 2 criterion and the line integral convolution (LIC) technique indicating sectional streamlines. The flow regions (coolant plenum, holes, and boundary layer) are studied subsequently and linked to each other. To track the anti-kidney vortex throughout the boundary layer, we propose two criteria which are based on vorticity and on LIC results. This enables us to associate the jet vortices with the cooling effectiveness at the wall, which is the key feature of film cooling. 展开更多
关键词 Film cooling anti-kidney vortex vortex identification trajectory tracking large-eddy simulation LES compound angle double row kidney vortex jet in cross-flow.
原文传递
不同制导律在脉冲式弹道修正灵巧弹上的应用
16
作者 葛健全 贾天宝 +2 位作者 张晓今 杨涛 寇保华 《弹箭与制导学报》 CSCD 北大核心 2008年第4期182-185,218,共5页
研究两种制导律在脉冲式弹道修正灵巧弹上的应用。建立基于零效脱靶量概念的两种末制导律——弹体追踪和脉冲比例导引,并给出对应的脉冲发动机点火控制方法。采用6自由度动力学模型进行仿真,计算结果表明在理想情况下文中方法可以实现... 研究两种制导律在脉冲式弹道修正灵巧弹上的应用。建立基于零效脱靶量概念的两种末制导律——弹体追踪和脉冲比例导引,并给出对应的脉冲发动机点火控制方法。采用6自由度动力学模型进行仿真,计算结果表明在理想情况下文中方法可以实现对地面固定目标精确打击。最后结合算例指出两种制导方案的特点,为总体设计提供有益的参考。 展开更多
关键词 弹道修正 脉冲发动机 零效脱靶量 弹体追踪 脉冲比例导引
下载PDF
THEORETICAL AND EXPERIMENTAL STUDIES OF THE FLARING GATE PIER ON THE SURFACE SPILLWAY IN A HIGH-ARCH DAM 被引量:11
17
作者 LI Nai-wen LIU Chao +1 位作者 DENG Jun ZHANG Xiao-zhe 《Journal of Hydrodynamics》 SCIE EI CSCD 2012年第4期496-505,共10页
The experimental studies of the flaring gate pier applied on the surface spillway in a high-arch dam show that a shock-wave will appear when the pattern of the flow is kept as super-critical. Meanwhile, the water dept... The experimental studies of the flaring gate pier applied on the surface spillway in a high-arch dam show that a shock-wave will appear when the pattern of the flow is kept as super-critical. Meanwhile, the water depth at the outlet increases significantly, the flow moves downward in different directions, and the plunging jet is in a narrow and long shape, with a full longitudinal diffusion. In addition, the variation of the flaring gate pier design parameters affects little the discharge capacity of the surface spillway, these parameters including the contraction ratio fl, the contraction angle c~ and the spillway chute angle O. The pressure on the bottom of the spillway increases along the way and reaches the maximum before the outlet, and then decreases rapidly. Due to the flow impacting, the pressure on both sidewalls increases abruptly at the turning line of the flaring gate pier. To see the characteristics of the flow in the flaring gate pier, a simple calculation method is suggested based on the conversation of energy and mass, and the calculation methods for the jet trajectory and the horizontal length in air are also proposed. The results are found in good agreement with experimental data. 展开更多
关键词 high-arch dam flood discharge and energy dissipation flaring gate pier hydraulic calculation jet trajectory distance
原文传递
高坝挑流消能述评 被引量:10
18
作者 潘瑞文 《云南水力发电》 1998年第3期15-19,共5页
本文针对影响挑流消能工设计选型的几个问题进行评述分析。指出:冲击射流的脉动作用是岩基局部冲刷破坏的主要因素;现有冲深估算公式均具有一定的局限性;挑坎体型优化的目标在于提高射流在空中的消能率,减小和分散入水冲击能量,改... 本文针对影响挑流消能工设计选型的几个问题进行评述分析。指出:冲击射流的脉动作用是岩基局部冲刷破坏的主要因素;现有冲深估算公式均具有一定的局限性;挑坎体型优化的目标在于提高射流在空中的消能率,减小和分散入水冲击能量,改善水垫消能的作用,从而减轻射流对下游的冲刷,确保泄洪安全,并注意顾及池洪雾化的不利影响。 展开更多
关键词 挑流消能 冲刷机理 高坝 消能方式
下载PDF
高海拔地区气压环境对高速水流水舌挑距的影响 被引量:10
19
作者 庞博慧 马洪琪 《水力发电学报》 EI CSCD 北大核心 2018年第2期88-95,共8页
我国西部高海拔地区低气压环境对高坝建设中高速水流的水力学特性研究提出了新的挑战。高速水流水舌挑距是影响水垫塘及岸坡安全性的关键技术指标。本文采用计算流体动力学分析方法研究环境气压对水舌挑距的影响程度,建立低气压环境下... 我国西部高海拔地区低气压环境对高坝建设中高速水流的水力学特性研究提出了新的挑战。高速水流水舌挑距是影响水垫塘及岸坡安全性的关键技术指标。本文采用计算流体动力学分析方法研究环境气压对水舌挑距的影响程度,建立低气压环境下水舌抛射距离的理论估算公式,为高海拔地区高速水流水舌挑距的分析提供参考。研究表明,环境气压越低,水舌挑距越远;环境气压每下降10 kPa,挑距基本呈增大约1.5%的趋势。为避免由于未考虑低气压影响水舌挑距预测偏小而导致的岸坡或水垫塘安全风险,建议在高山峡谷区水垫塘紧凑布置时应充分考虑低气压对水舌挑距的影响。 展开更多
关键词 工程水力学 水舌挑距 计算流体动力学 低气压环境 高海拔
原文传递
溢洪道消能方案研究进展 被引量:10
20
作者 张建军 《科技情报开发与经济》 2009年第29期120-121,共2页
将国内外有关溢洪道消能方案的研究成果进行了归纳和总结,着重探讨了挑流消能、底流消能和阶梯溢洪道消能,并介绍了一些新型的消能方案和模型试验成果。
关键词 溢洪道消能 挑流消能 底流消能 阶梯溢洪道消能
下载PDF
上一页 1 2 3 下一页 到第
使用帮助 返回顶部