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Effects of vegetation patch density on flow velocity characteristics in an open channel 被引量:12
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作者 Wen-qi Li Dan Wang +1 位作者 Jun-li Jiao Ke-jun Yang 《Journal of Hydrodynamics》 SCIE EI CSCD 2019年第5期1052-1059,共8页
The aquatic plants are often found in natural rivers,and they affect the channel flow structure significantly.To study the effects of the vegetation density a(the frontal area per volume)on the flow velocity character... The aquatic plants are often found in natural rivers,and they affect the channel flow structure significantly.To study the effects of the vegetation density a(the frontal area per volume)on the flow velocity characteristics,rigid bamboo circular cylinders are chosen as the model emergent vegetation.In the experiments,the density of the vegetation takes various values while all other flow parameters are kept constant.A 3-D acoustic Doppler velocimeter(ADV)is used to measure the local flow velocities for different vegetation densities.The results show that the existence of the vegetation patch leads to an increase of the depth-averaged velocity on the right and left sides behind the vegetation patch,and it increases monotonically with the vegetation density.For different vegetation densities,the lateral distribution of the stream-wise velocity behind the vegetation patch follows approximately an S-shaped profile when a≤60 m-1,and a logarithmic profile if a>60 m-1.The vertical distribution of the stream-wise velocity along the channel varies with the vegetation density and also follows an S-shaped distribution in a certain range,with the locations and the ranges being affected by the vegetation density. 展开更多
关键词 VEGETATION density stream-wise VELOCITY depth-averaged VELOCITY lateral DISTRIBUTION longitudinal DISTRIBUTION open channel
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CURVED OPEN CHANNEL FLOW ON VEGETATION ROUGHENED INNER BANK 被引量:7
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作者 HUAI Wen-xin LI Cheng-guang +2 位作者 ZENG Yu-hong QIAN Zhong-dong YANG Zhong-hua 《Journal of Hydrodynamics》 SCIE EI CSCD 2012年第1期124-129,共6页
A RNG numerical model together with a laboratory measurement with Micro ADV are adopted to investigate the flow through a 180o curved open channel(a 4 m straight inflow section,a 180o curved section,and a 4m straight... A RNG numerical model together with a laboratory measurement with Micro ADV are adopted to investigate the flow through a 180o curved open channel(a 4 m straight inflow section,a 180o curved section,and a 4m straight outflow section)partially covered with rigid vegetations on its inner bank.Under the combined action of the vegetation and the bend flow,the flow structure is complex.The stream-wise velocities in the vegetation region are much smaller than those in the non-vegetation region due to the retardation caused by the vegetation.For the same reason,no clear circulation is found in the vegetated region,while in the non-vegetation region,a slight counter-rotating circulation is found near the outer bank at both 90o and downstream curved cross-sections.A comparison between the numerical prediction and the laboratory measurement shows that the RNG model can well predict the flow structure of the bend flow with vegetation.Furthermore,the shear stress is analyzed based on the numerical prediction.The much smaller value in the inner vegetated region indicates that the vegetation can effectively protect the river bank from scouring and erosion,in other words,the sediment is more likely to be deposited in the vegetation region. 展开更多
关键词 RNG numerical model non-submerged rigid vegetation bend flow stream-wise velocities shear stress
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Effects of Staged Injection on Supersonic Mixing and Combustion 被引量:6
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作者 HOU Lingyun Bernhard WEIGAND Marius BANICA 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第5期584-589,共6页
The three-dimensional (3D) reacting flow in a staged supersonic combustor is examined numerically. In order to obtain the optimum stream-wise vortices, a swept ramp injector is chosen as the second-stage wall inject... The three-dimensional (3D) reacting flow in a staged supersonic combustor is examined numerically. In order to obtain the optimum stream-wise vortices, a swept ramp injector is chosen as the second-stage wall injection combined with the first-stage central strut injection. The performance of the two-staged injection is compared with that of a one-staged injection, while the strut is kept installed in both cases. The two-staged injections can make full use of the residual oxygen near the wall and release more heat. The second-stage injection further downstream avoids the strong shock waves in the isolator and results in a rising wall pressure and good burning effects after the wall injection. Therefore, it allows more fuel to be injected into the supersonic combustor without causing thermal choking. Parallel injection from the second-stage swept ramp shows low total pressure loss and the best burning efficiency, compared with the other injection angles. 展开更多
关键词 supersonic mixing stream-wise vortices staged injection swept ramp COMBUSTION
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EXPERIMENTAL STUDY ON TURBULENT BOUNDARY LAYER CHARACTERISTICS OVER STREAMWISE RIBLETS 被引量:5
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作者 ZHAOZhi-yong DONGShou-ping DUYa-nan 《Journal of Hydrodynamics》 SCIE EI CSCD 2004年第3期350-355,共6页
Measurements of characteristics by means of a two-component Laser DopplerVelocimeter (LDV) were carried out in turbulent boundary layers over both a symmetric V-shapedribbed plate and a smooth one in a low speed wind ... Measurements of characteristics by means of a two-component Laser DopplerVelocimeter (LDV) were carried out in turbulent boundary layers over both a symmetric V-shapedribbed plate and a smooth one in a low speed wind tunnel. The present results clearly indicate thatthe logarithmic velocity profile over the riblets surface is shifted upward with a 30. 9% increasein the thickness of the viscous sublayer. Also a change in the log-law region is found. And themaximum value of streamwise velocity fluctuations is reduced by approximately 17%. The skewness andflatness factors do not show any change besides those in the region of y^+ 【 0. 6 . It is evidentthat the Reynolds shear stress over the riblets is reduced. Further more, in log-law region, theReynolds shear stress has a larger reduction of up to 18%. 展开更多
关键词 laser doppler velocimeter (LDV) stream-wise riblets turbulent boundarylayer turbulence fluctuations characteristics
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Flow-Induced Stream-Wise Vibration of Circular Cylinders
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作者 Atsushi Okajima Takahiro Kiwata 《Journal of Flow Control, Measurement & Visualization》 2019年第3期133-151,共19页
Results from a series of studies on the stream-wise vibration of a circular cylinder verifying Japan Society of Mechanical Engineers Standard S012-1998, Guideline for Evaluation of Flow-induced Vibration of a Cylindri... Results from a series of studies on the stream-wise vibration of a circular cylinder verifying Japan Society of Mechanical Engineers Standard S012-1998, Guideline for Evaluation of Flow-induced Vibration of a Cylindrical Structure in a Pipe, are summarized and discussed in this paper. Experiments were carried out in a water tunnel and in a wind tunnel using a two-dimensional cylinder model elastically supported at both ends of the cylinder and a cantilevered cylinder model with a finite span length that was elastically supported at one end. These cylinder models were allowed to vibrate with one degree of freedom in the stream-wise direction. In addition, we adopted a cantilevered cylinder model that vibrated with two degrees of freedom in both the stream-wise and cross-flow directions under the same vibration conditions as an actual thermocouple well. The value of the Scruton number (structural damping parameter) was changed over a wide range, so as to evaluate the value of the critical Scruton number that suppressed vibration of the cylinder. For the two-dimensional cylinder, two different types of stream-wise excitations appeared in the reduced velocity range of approximately half of the resonance-reduced velocity. For the stream-wise vibration in the first excitation region, due to a symmetric vortex flow, the response amplitudes were sensitive to the Scruton number, while the shedding frequency of alternating vortex flow was locked-in to half of the Strouhal number of vibrating frequency of a cylinder in the second excitation region. In addition, the effects of the aspect ratio of a cantilevered cylinder on the flow-induced vibration characteristics were clarified and compared with the results of a two-dimensional cylinder. When a cantilevered circular cylinder with a finite length vibrates with one degree of freedom in the stream-wise di-rection, it is found that acylinder with a small aspect ratio has a single excitation region, whereas a cylinder with a large aspect ratio has two excitation regions. Furthe 展开更多
关键词 Flow-Induced VIBRATION Flow Visualization Bluff Body Circular Cylinder Scruton Number Finite Spanlength ASPECT Ratio stream-wise VIBRATION CROSS-FLOW VIBRATION One and Two Degrees of FREEDOM
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非等温流向振荡单圆柱绕流的格子Boltzmann模拟
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作者 包胜 陈胜 +2 位作者 柳朝晖 易超 郑楚光 《工程热物理学报》 EI CAS CSCD 北大核心 2012年第7期1181-1184,共4页
本文采用格子Boltzmann方法模拟对非等温横向振荡圆柱绕流(Re=100)进行模拟,详细考察振荡频率(F=f_o/f_s=0.2~8.0)、振幅(A/D=0.1~0.4,A为圆柱流向最大位移,D为圆柱直径)对绕流换热的影响。结果表明:低频率、低振幅流向振荡运动将使... 本文采用格子Boltzmann方法模拟对非等温横向振荡圆柱绕流(Re=100)进行模拟,详细考察振荡频率(F=f_o/f_s=0.2~8.0)、振幅(A/D=0.1~0.4,A为圆柱流向最大位移,D为圆柱直径)对绕流换热的影响。结果表明:低频率、低振幅流向振荡运动将使圆柱换热增强,高频率、高振幅振荡使圆柱换热效果减弱;圆柱表面平均N_u脉动均方根值随着振荡频率、振幅的增大而增大;在锁定区域内,平均N_u及其脉动均方根值均出现极大值。 展开更多
关键词 流向振荡 非等温 格子BOLTZMANN Nu数 频谱分析
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Effects of a Kind of Non-smooth Blade on the Unsteady Flow Field at the Exit of an Axial Fan
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作者 Hongwei MA Jibo GUO 《Journal of Thermal Science》 SCIE EI CAS CSCD 2008年第1期1-6,共6页
An experimental investigation of effects of a kind of streamwise-grooved blade on the unsteady flow field at an exit of an axial-flow fan was performed. The flow field at 25% chord downstream from the trailing edge at... An experimental investigation of effects of a kind of streamwise-grooved blade on the unsteady flow field at an exit of an axial-flow fan was performed. The flow field at 25% chord downstream from the trailing edge at hub was measured using a fast-response five-hole pressure probe at different mass-flow conditions. The unsteady flow of the grooved blades was compared with that of the smooth blades. The measurement results indicate that: (1) the grooved blades restrain the velocity fluctuation and the pressure fluctuation by modulating the blade boundary layers, which contributes to the flow loss reduction in the hub region and in the rotor wake region at the design condition; (2) the stream-wise grooves play an important role in restraining the radial migration in the blade boundary layer and abating the tip flow mixing, which contributes to the flow loss reduction in the tip region at the design condition; (3) at the near stall condition, the grooved surface can not reduce the flow loss, even increase the loss nearby when the separation happens in the blade boundary layer. 展开更多
关键词 axial fan non-smooth blade stream-wise groove unsteady flow.
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Numerical simulation of VIV for an elastic cylinder mounted on the spring supports with low mass-ratio
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作者 徐俊凌 朱仁庆 《Journal of Marine Science and Application》 2009年第3期237-245,共9页
With the development of the offshore deep water oil industry many researchers are focusing on the vortex-induced vibrations (VIV) of deep risers. In the present work, Reynolds-averaged Navier-Stokes (RANS) equatio... With the development of the offshore deep water oil industry many researchers are focusing on the vortex-induced vibrations (VIV) of deep risers. In the present work, Reynolds-averaged Navier-Stokes (RANS) equations were combined with the SST κ-ω turbulent model to simulate the stream-wise and transverse motion of an elastically mounted cylinder with a low mass-ratio, a natural frequency ratio of fx/fy = 1 and an Re number between 5 300 and 32 000, The four-order Runge-Kutta method was applied to solve the oscillating equation of the cylinder. The relationship between reduced velocity and parameters of the cylinder, including the lift coefficient, the drag coefficient, displacement and the vortex structure were then compared with recent experimental results and discussed in detail. The present numerical simulation reproduced effects have been observed in experiments, such as the lock-in phenomenon, the hysteretic phenomenon and beating behavior. 展开更多
关键词 VIV low mass ratio stream-wise and transverse motion TWO-DEGREE-OF-FREEDOM vortex shedding model CFD
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两向自由度低质量比圆柱体涡激振动的数值计算 被引量:32
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作者 黄智勇 潘志远 崔维成 《船舶力学》 EI 北大核心 2007年第1期1-9,共9页
使用RANS方程求解器结合SST k-ω湍流模型对低质量比弹性支撑圆柱体在流向和横向(两向)的运动进行了数值计算,着重研究了限制流向运动与否对圆柱体横向振幅的影响。通过对不同质量比圆柱体在较大折合速度范围内的计算,得出了当质量比低... 使用RANS方程求解器结合SST k-ω湍流模型对低质量比弹性支撑圆柱体在流向和横向(两向)的运动进行了数值计算,着重研究了限制流向运动与否对圆柱体横向振幅的影响。通过对不同质量比圆柱体在较大折合速度范围内的计算,得出了当质量比低于m*cri=3.5时,两向自由度的圆柱体比限制流向运动的圆柱体能产生更大的横向振幅。数值计算结果与最近物理实验结果进行了详细的比较和讨论。 展开更多
关键词 涡激振动 低质量比 计算流体动力学 流向和横向运动
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波瓣喷管引射-混合器涡结构的数值研究 被引量:13
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作者 单勇 张靖周 《空气动力学学报》 EI CSCD 北大核心 2005年第3期355-359,共5页
通过波瓣喷管引射-混合器的流场三维数值计算,得到了流向涡和正交涡产生、衰减的演变以及对混合效率的影响规律,进一步揭示了波瓣喷管有利于强化引射能力和混合效率的内在机理。结果表明:喷管出口流向涡的尺度基本与波瓣的高度相当,流... 通过波瓣喷管引射-混合器的流场三维数值计算,得到了流向涡和正交涡产生、衰减的演变以及对混合效率的影响规律,进一步揭示了波瓣喷管有利于强化引射能力和混合效率的内在机理。结果表明:喷管出口流向涡的尺度基本与波瓣的高度相当,流向涡可以诱发主流和次流之间强烈的对流混合,在喷管下游一倍混合管直径的混合距离内强化混合作用显著,随着流向涡向下游发展,涡强衰减迅速;正交涡具有与波瓣尾缘一样的几何外形,在混合管下游,由于主流和次流之间的速度梯度下降,正交涡的强度显著降低,对强化混合的影响不大。 展开更多
关键词 波瓣喷管 混合器 数值计算 流向涡 正交涡
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有植被明渠纵向流速垂向分布特性的PIV试验分析 被引量:16
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作者 槐文信 赵磊 +1 位作者 李丹 李琼 《实验流体力学》 EI CAS CSCD 北大核心 2009年第1期26-30,共5页
有植被河道水流的流速分布是确定植被河道阻力和过流能力的基础。在室内矩形断面水槽中模拟了有树桩存在的河流环境,采用粒子图像速度仪(PIV)测量了同一流量情况下,非淹没及淹没刚性植被稳恒流纵向流速垂向分布。试验结果表明矩形断面... 有植被河道水流的流速分布是确定植被河道阻力和过流能力的基础。在室内矩形断面水槽中模拟了有树桩存在的河流环境,采用粒子图像速度仪(PIV)测量了同一流量情况下,非淹没及淹没刚性植被稳恒流纵向流速垂向分布。试验结果表明矩形断面非淹没刚性植被水流时空平均纵向流速垂向分布符合'J'形分布,淹没刚性植被水流时空平均纵向流速垂向分布符合'S'形分布,植被中不同位置垂线的时均纵向流速分布不同。笔者给出的流速资料可作为植被水流数值模拟对比的参考。 展开更多
关键词 纵向流速分布 PIV 非淹没植被 淹没植被
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基于掺长理论的淹没柔性植被水流流速分布研究 被引量:15
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作者 槐文信 韩杰 +2 位作者 曾玉红 安翔 钱忠东 《应用数学和力学》 CSCD 北大核心 2009年第3期325-332,共8页
采用PVC薄片对柔性植被进行了模拟,并用三维Micro ADV对淹没柔性植被恒定水流进行了实验测量,获得了水流纵向流速和Reynolds切应力的分布.实验结果表明,淹没柔性植被水流植被层和非植被层的水力特性有显著不同.在非植被层,Reynolds应力... 采用PVC薄片对柔性植被进行了模拟,并用三维Micro ADV对淹没柔性植被恒定水流进行了实验测量,获得了水流纵向流速和Reynolds切应力的分布.实验结果表明,淹没柔性植被水流植被层和非植被层的水力特性有显著不同.在非植被层,Reynolds应力为直线分布,而时均流速则符合经典的对数律分布.基于新"河床"的概念,首次提出用河道压缩参数来表示植被对水流的影响,并合理假设了一个新的混合长度公式,由此得到的时均流速公式相比前人的成果有所需参数少、计算简单及实用性强等优点. 展开更多
关键词 柔性植被 PVC薄片 MICRO ADV(多普勒超声测速仪) 混合长度 主流流速分布 Reynolds应力 河道压缩参数
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流向涡与涡轮叶栅二次流相互作用研究 被引量:8
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作者 王鹏 邹正平 +2 位作者 綦蕾 刘火星 叶建 《实验流体力学》 EI CAS CSCD 北大核心 2010年第3期42-49,共8页
研究有效的流动控制手段,降低涡轮内部二次损失,对于小展弦比涡轮的气动设计具有重要意义。利用涡发生器在叶栅入口前产生流向涡,通过试验和数值方法探讨这种基于旋涡相互作用的流动控制方法对涡轮平面叶栅二次流动的作用效果,并对不同... 研究有效的流动控制手段,降低涡轮内部二次损失,对于小展弦比涡轮的气动设计具有重要意义。利用涡发生器在叶栅入口前产生流向涡,通过试验和数值方法探讨这种基于旋涡相互作用的流动控制方法对涡轮平面叶栅二次流动的作用效果,并对不同流向涡情况做对比分析。结果表明:流向涡对涡轮叶栅内部流动会产生较为显著的影响,从而影响叶栅的性能,当所产生流向涡强度和位置较为合理时,有可能通过流向涡与二次流的相互作用达到较大幅度降低二次流损失的目的。 展开更多
关键词 二次流 流动控制 流向涡 涡发生器 气动损失
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波瓣数对波瓣S型混合二元喷管气动热力性能影响 被引量:6
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作者 杜力伟 刘友宏 +2 位作者 邵万仁 徐速 邓洪伟 《航空动力学报》 EI CAS CSCD 北大核心 2015年第4期916-926,共11页
依据某型涡扇发动机波瓣S型混合二元喷管,保持波瓣混合器长度、内扩张角、外扩张角以及宽高比不变,依次取波瓣混合器波瓣数为12,14,16,18,20,建立了一组具有不同波瓣数的波瓣S型混合二元喷管模型.采用经过验证的CFD方法,研究了波瓣数对... 依据某型涡扇发动机波瓣S型混合二元喷管,保持波瓣混合器长度、内扩张角、外扩张角以及宽高比不变,依次取波瓣混合器波瓣数为12,14,16,18,20,建立了一组具有不同波瓣数的波瓣S型混合二元喷管模型.采用经过验证的CFD方法,研究了波瓣数对波瓣S型混合二元喷管气动热力性能的影响规律.结果表明:在波瓣尾缘截面至第1个S弯截面区域,波瓣数对流体混合程度产生很大影响,并且热混合效率近乎随波瓣数增加而增加.在第1个S弯截面至波瓣S型混合二元喷管出口截面区域,波瓣数为16的波瓣S型混合二元喷管模型的总压恢复系数始终最低,其余模型的总压恢复系数以及热混合效率没有明显差别.在波瓣S型混合二元喷管出口截面上,波瓣数为16的波瓣S型混合二元喷管模型的热混合效率最高,达到0.850,然而其总压恢复系数相对于该截面上最高值下降了0.289%.此外,波瓣S型混合二元喷管的渐缩型流道能够提高流向涡强迫混合效果,但同时也加速流向涡的耗散速率. 展开更多
关键词 波瓣混合器 波瓣S型混合二元喷管 波瓣数 流向涡 热混合效率 总压恢复系数
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仿生波浪前缘叶片在核电汽轮机中的应用 被引量:4
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作者 陈桐 谢诞梅 +4 位作者 杨长柱 张恒良 熊扬恒 杜海芬 张敬 《中国电机工程学报》 EI CSCD 北大核心 2018年第12期3605-3612,共8页
采用数值模拟的方法研究了仿生波浪前缘对某型核电汽轮机高压末级变工况特性的影响,分析了蒸汽在仿生波浪前缘叶栅内的流动机理。通过研究发现,在所研究的汽轮机级输出功率变化范围内,具有波浪前缘改型动叶栅的核电汽轮机末级相比原型... 采用数值模拟的方法研究了仿生波浪前缘对某型核电汽轮机高压末级变工况特性的影响,分析了蒸汽在仿生波浪前缘叶栅内的流动机理。通过研究发现,在所研究的汽轮机级输出功率变化范围内,具有波浪前缘改型动叶栅的核电汽轮机末级相比原型具有更高的相对内效率。并且,随汽轮机级输出功率的降低,级效率提升幅度相应增大。当级负荷降低至12.5%时,级效率可提高3%。经流动可视化分析,发现动叶栅波浪前缘形成的流向涡结构是造成效率提高的主要原因,在涡结构的生长、延伸、耗散过程中,促进了叶片边界层内流体与主流间的能量交换,从而减小边界层损失。 展开更多
关键词 汽轮机 叶片 波浪前缘 变工况 数值模拟 流向涡
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高频阵列式能量沉积对超燃燃烧室性能影响的数值研究
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作者 蔡子林 高峰 +1 位作者 王宏宇 马岑睿 《航空兵器》 CSCD 北大核心 2023年第3期80-86,共7页
超声速来流具有较大的动量,致使横向射流受来流强压缩的影响难以具有较大的穿透深度,影响了射流在超燃燃烧室中的掺混效率。本文提出了利用能量沉积力、热扰动来辅助提升射流掺混效率的方法,并开展了数值模拟研究。通过求解带能量源项... 超声速来流具有较大的动量,致使横向射流受来流强压缩的影响难以具有较大的穿透深度,影响了射流在超燃燃烧室中的掺混效率。本文提出了利用能量沉积力、热扰动来辅助提升射流掺混效率的方法,并开展了数值模拟研究。通过求解带能量源项和化学反应源项的N-S方程,对比分析了施加在射流前和射流后的两种高频阵列式能量沉积分布方式对带凹腔的超燃燃烧室的影响。研究发现,能量沉积由于增大了射流诱导流向涡的尺度,可提升燃烧室乙烯燃料的掺混性能;能量沉积可提升燃烧室的燃烧效率,且分布在射流后方时燃烧效率较高,相比于基准工况提高了29%;能量沉积的加入略微降低了燃烧室总压恢复系数。 展开更多
关键词 超燃燃烧室 能量沉积 流向涡 掺混 燃料喷注 总压恢复系数 冲压发动机
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叶轮机转子内流动的三维跨声速Navier-Stokes方程组数值计算及试验验证 被引量:3
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作者 魏玲 葛宁 《空气动力学学报》 CSCD 北大核心 2005年第3期350-354,359,共6页
应用有限体积法及Baldwin-Lomax代数湍流模型求解叶轮机转子内流动的三维可压缩非定常薄层Navier-Stokes方程组,计算一个绕X轴等转速旋转的转子内流场问题,用当地时间步长方法来加速收敛。采用隐式算法对对流通量进行求解,而耗散通量采... 应用有限体积法及Baldwin-Lomax代数湍流模型求解叶轮机转子内流动的三维可压缩非定常薄层Navier-Stokes方程组,计算一个绕X轴等转速旋转的转子内流场问题,用当地时间步长方法来加速收敛。采用隐式算法对对流通量进行求解,而耗散通量采用显式算法。采用高阶TVD下的Roe格式计算对流通量,采用中心差分格式计算耗散通量。关于守恒变量Q的非线性方程组,采用牛顿迭代方法求解,线化后的方程用对称的Gauss-Seidle方法求其渐近解。应用该算法模拟了转子Rotor67流场,与试验做了大量的对比研究,包括性能、等马赫线以及总压和总温等。在最高效率点附近计算与试验比较接近,但在靠近失速点时计算与试验有较大的差别。 展开更多
关键词 压气机 数值模拟 试验验证 旋转坐标系
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超声速燃烧室内氢气燃烧的三维数值研究 被引量:2
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作者 周建兴 朴英 +1 位作者 岂兴明 祝剑虹 《航空动力学报》 EI CAS CSCD 北大核心 2007年第12期1984-1988,共5页
通过隐式耦合求解可压缩N-S方程及组分方程,对氢气的超声速燃烧进行三维数值模拟,对燃烧室内的冷热态流场,以及氢气喷射压力对燃烧的影响进行了系统分析和研究.研究表明,燃烧放热以及氢气喷射压力提高都会导致燃烧室内波系结构变化,沿... 通过隐式耦合求解可压缩N-S方程及组分方程,对氢气的超声速燃烧进行三维数值模拟,对燃烧室内的冷热态流场,以及氢气喷射压力对燃烧的影响进行了系统分析和研究.研究表明,燃烧放热以及氢气喷射压力提高都会导致燃烧室内波系结构变化,沿周向的流向涡增强,压缩波和膨胀波与氢气核心区的相互作用增强,促进氢气和空气的掺混,更利于氢气的燃烧. 展开更多
关键词 航空 航天推进系统 超声速燃烧 氢气 流向涡 超燃冲压发动机
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马赫数2.5超/亚声流流向涡掺混超燃室冷态实验 被引量:3
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作者 介克 杨占宇 +4 位作者 赵吕顺 刘建 王洪铭 黄勇 单鹏 《航空动力学报》 EI CAS CSCD 北大核心 2007年第12期2012-2017,共6页
结合对应的数值计算,对一种带亚声速预燃室和流向涡掺混器的超声速燃烧模型燃烧室实验台,在其进口马赫数为2.5的来流条件下,进行了冷态流场的实验研究.实验测得其壁面静压分布和激波系结构与流场的CFD计算结果基本一致.实验结果表明,模... 结合对应的数值计算,对一种带亚声速预燃室和流向涡掺混器的超声速燃烧模型燃烧室实验台,在其进口马赫数为2.5的来流条件下,进行了冷态流场的实验研究.实验测得其壁面静压分布和激波系结构与流场的CFD计算结果基本一致.实验结果表明,模型燃烧室全流场超声速,达到设计状态.马赫数2.5下的冷态实验数据和CFD计算数据为进行点火实验提供了依据. 展开更多
关键词 航空 航天推进系统 超声速燃烧 预燃室 波瓣掺混器 流向涡掺混
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非光滑叶片对轴流风扇气动性能的影响 被引量:2
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作者 郭继波 马宏伟 《工程热物理学报》 EI CAS CSCD 北大核心 2007年第3期406-408,共3页
在低速轴流风扇实验台上,通过对比测量光滑转子叶片、两种表面具有流向沟槽的非光滑转子叶片风扇的气动性能,研究了叶片沟槽面对风扇气动性能的影响。结果表明:(1)在设计状态和小流量状态,采用微槽型非光滑叶片能提高该风扇的流量、降... 在低速轴流风扇实验台上,通过对比测量光滑转子叶片、两种表面具有流向沟槽的非光滑转子叶片风扇的气动性能,研究了叶片沟槽面对风扇气动性能的影响。结果表明:(1)在设计状态和小流量状态,采用微槽型非光滑叶片能提高该风扇的流量、降低总压损失和提高风扇总压升;(2)在近失速状态,非光滑叶片使风扇性能下降;(3)非光滑叶片对风扇性能的影响在很大程度上取决于非光滑叶片的沟槽尺寸。 展开更多
关键词 轴流风扇 非光滑叶片 流向微槽 气动性能
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