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湍动槽中采用层析粒子成像测速技术来测量耗散元素检测方案(粒子图像测速)

A new method to describe small scale statistical information from passive scalar fields has been proposed by Wang and Peters (2006). They used direct numerical simulations (DNS) of homogeneous shear flow to introduce the innovative concept. This novel method determines the local minimum and maximum points of a fluctuating scalar field via gradient trajectories starting from every grid point in the direction of the steepest ascending and descending scalar gradients. Relying on gradient trajectories, a dissipation element is defined as the region of all the grid points the trajectories of which share the same pair of maximum and minimum points. The procedure has also been successfully applied to various DNS fields of homogeneous shear turbulence using the three velocity components and the kinetic energy as scalar fields. To validate statistical properties of these elements derived from DNS (Wang and Peters 2006, 2008), dissipation elements are for the first time determined based on experimental data of a fully developed turbulent channel flow. The dissipation elements are deduced from the gradients of the instantaneous fluctuation of the three velocity components u5, v5, and w5 and the instantaneous kinetic energy k5, respectively. The required 3D velocity data is obtained investigating a 17.82 × 17.82 × 2.7 mm3 (0.356  × 0.356  × 0.054 ) test volume using tomographic particle-image velocimetry (Tomo-PIV). The measurements are conducted at a Reynolds number of 1.7× 104 based on the channel half-height  and the bulk velocity U. Detection and analysis of dissipation elements from the experimental velocity data are presented. The statistical results are compared to the DNS data from Wang and Peters (2006, 2008).
检测样品: 其他
检测项: 采用层析粒子成像测速技术来测量耗散元素

北京欧兰科技发展有限公司

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喷雾,燃料中浓度场检测方案(尾气检测)

To understand and optimize the combustion processes in new types of internal combustion engines, like gasoline direct-injection engines, non-intrusive laser-based diagnostics methods have proven to be versatile and important tools to measure combustion characteristics. Most engine developers already rely on optical methods in the development of new engines. To guarantee accurate and reliable results of optical measurements it is necessary to carefully evaluate and characterize these techniques under realistic conditions. In this work a variety of laser-based diagnostics techniques, mostly based on the tracer- LIF principle, have been evaluated for their applicability and limitations and have been applied to different spray systems – reaching from single droplets, over model sprays to fuel sprays in a firing test engine. The tracer-laser-induced-fluorescence (LIF) method is based on doping the fuel with a fluorescent substance whose fluorescence characteristics are used to measure various physical properties of the spray, such as temperature, droplet size, or droplet velocity. From these properties information about heat and mass-transfer mechanisms in the spray can be gained. However, the characteristics of the used tracers must be known in detail in order to guarantee useful and comparable results. Therefore, in this work various tracers were characterized in terms of their evaporation and temperaturedependent properties. The tracers Atto 680, Rhodamine 800 and Rhodamine B have further been tested for their applicability to realistic fuels.
检测样品: 其他
检测项: 浓度场

北京欧兰科技发展有限公司

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鱼道中2D非稳定流动实验研究检测方案(粒子图像测速)

Vertical slot fish passes have been applied as a solution to mitigate fish migration problems in running waters, for over two decades. They are commonly used to enable target fish to ascend through obstacles in rivers. However, small species are rarely considered in such fishways, of which the performance for small fish still remains unknown. This experiment was to study the turbulence structure in a vertical slot fish pass concerning two different pool length/width ratios of 9 and 6.67 as well as the effect of installing a cylinder behind the slot in affecting the characteristics of instationary flow. Cylinders are considered an effective solution to modify the flow structure and to reduce velocity and turbulent energy in order to adapt the flow for the passage of small fish species. Flow visualization and particle image velocimetry were used to study the characteristics of mean flow and turbulence and particular emphasis on the unsteady flow. The results show that flow patterns consist of a water jet and one or two recirculation zones depending on the length/width ratio of the pool. The direction of the jet was strongly affected by the vertical cylinders. The frequencies and spatio-temporal evolutions of the main jet beats were analyzed. Combining with the previous studies of fish migration experiments, the results provide hydraulic evidence on the biological performance.
检测样品: 其他
检测项: 2D非稳定流动实验研究

北京欧兰科技发展有限公司

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环形喷嘴中利用声激发主动控制大直径比初始区域环形不稳定性检测方案(粒子图像测速)

Proper Orthogonal Decomposition (P.O.D.) is a technique used for analysis of vortex structures in a turbulent flow. In this study, complex shear flows are observed by P.I.V. measurements (Particle Image Velocimetry) of a large diameter ratio annular jet. The annular jet is an example of complex shear flow situations. Two axisymmetric shear layers, originating at the jet exit, one at the nozzle lip and the other at the centre body, eventually meet downstream or interact with each other. The main aim of this study is to observe and analyze the effects of active control using acoustic waves on an annular jet with a great diameter ratio (r= 0.91), in order to find a new way to reduce jet instabilities. This contribution discusses the application of Proper Orthogonal Decomposition to the P.I.V. (Particle Image Velocimetry) velocity fields of an annular jet and on a statistic of time resolved tomographic images of the initial zone of the annular jet. Acoustic waves are then applied on the annular jet with different frequencies (fundamental, first harmonic̷). Measurements are conducted with a Reynolds number ReDo=107800. The fluctuation frequency of the stagnation point is known for this Reynolds number. The Strouhal number corresponding to this frequency is StDo = 0.27. The P.O.D. analysis applied on a natural annular jet and an excited annular jet enables us to see the importance of the triggering of the acoustic wave with the stagnation point motion. An active control is therefore necessary to use acoustic excitation to reduce instabilities in the initial zone of these turbulent jets. Active control has already been used with round jets and has given promising results, but only a few studies have been conducted on annular jets in this field. This work will permit us essentially to have a better knowledge of annular jets and to meet manufacturers' needs.
检测样品: 其他
检测项: 利用声激发主动控制大直径比初始区域环形不稳定性

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