Instantaneous and time-averaged flow structures around a blunt double-cone with or without supersonic film cooling visualized via nano-tracer planar laser scattering

In a Mach 3.8 wind tunnel, both instantaneous and time-averaged flow structures of different scales around a blunt double-cone with or without supersonic film cooling were visualized via nano-tracer planar laser scattering (NPLS), which has a high spatiotemporal resolution. Three experimental cases with different injection mass flux rates were carried out. Many typical flow structures were clearly shown, such as shock waves, expansion fans, shear layers, mixing layers, and turbulent boundary layers. The analysis of two NPLS images with an interval of 5 μs revealed the temporal evolution characteristics of flow structures. With matched pressures, the laminar length of the mixing layer was longer than that in the case with a larger mass flux rate, but the full covered region was shorter. Structures like K-H (Kelvin-Helmholtz) vortices were clearly seen in both flows. Without injection, the flow was similar to the supersonic flow over a backward-facing step, and the structures were relatively simpler, and there was a longer laminar region. Large scale structures such as hairpin vortices were visualized. In addition, the results were compared in part with the schlieren images captured by others under similar conditions.     

Experimental study on supersonic film cooling on the surface of a blunt body in hypersonic flow

The experimental study focuses on the heat flux on a double cone blunt body in the presence of tangential-slot super- sonic injection into hypersonic flow. The tests are conducted in a contoured axisymmetric nozzle with Mach numbers of 7.3 and 8.1, and the total temperature is about 900 K. The injection Mach number is 3.2, and total temperature is 300 K. A constant voltage circuit is developed to supply the temperature detectors instead of the normally used constant current circuit. The schlieren photographs are presented additionally to visualize the flow and help analyze the pressure relationship between the cooling flow and the main flow. The dependence of the film-cooling effectiveness on flow parameters, i.e. the blow ratio, the convective Mach number, and the attack angle, is determined. A semi-empirical formula is tested by the present data, and is improved for a better correlation.     

连续波DF/HF化学激光器气膜冷却式喷管流场数值分析

在连续波DF/HF化学激光器主喷管收缩段采用气膜冷却方式,从3维离散小孔注入氦气射流以隔离壁面和主气流。通过对3种气膜孔排布方式下喷管内主气流状态进行数值模拟研究,分析氦气与主气流之间的相互作用,比较了不同方式下主气流氟原子冻结效率及壁面冷却效果。考虑到DF/HF化学激光器主喷管结构尺寸较小,采用适当间隔的单排圆孔注入是现实可行的,并有望达到较好的冷却保护效果,从而提高激光器运转效率。     

Effect of impingement jet on the full-coverage film cooling system with double layered wall

The present study was conducted to evaluate the total cooling effectiveness in combined full-coverage film cooling and impingement jet using an infrared thermographic technique. The effect of film cooling hole angle, blowing ratio, and height to diameter ratio between the film cooling and impingement jet plates was discussed. The total cooling effectiveness increased as impingement jet cooling was added. The angled film cooling holes had approximately 4.6% higher total cooling effectiveness than the normal film cooling holes. The total cooling effectiveness was almost constant regardless of height to diameter ratio, but enhanced as the blowing ratio was increased.     

周期性压力波动对气膜孔流动特性影响的研究

针对主流周期性压力波动的非稳态气膜冷却现象,分别采用非稳态及准稳态数值模拟进行了计算,通过对比揭示了非稳态气膜冷却现象的特征。结果表明:相对于主流的压力波动,气膜孔出口受到上一个时刻压力的影响,呈现出了波动延迟特性;针对本文所研究的波形特点,压力波动一方面导致压差(二次流与主流压力差值)变化无法快速直接地影响到二次流流动,阻止了倒流的发生,使得二次流流量更加稳定;另一方面,其携带的压力波动效应使得气膜孔出口形成贴壁性较好的环向外旋涡,将喷射出去的二次流重新带回壁面,使得二次流贴敷壁面。对于某一特定的主流波动特性而言,是存在在最佳设计长径比使得气膜孔质量流量特性及防止倒流特性达到最佳。本文研究对于涡轮周期性压力波动作用下的气膜孔气膜冷却研究具有较大的意义。     

连续波DF/HF化学激光器气膜冷却式喷管流场数值分析

在连续波DF/HF化学激光器主喷管收缩段采用气膜冷却方式,从3维离散小孔注入氦气射流以隔离壁面和主气流。通过对3种气膜孔排布方式下喷管内主气流状态进行数值模拟研究,分析氦气与主气流之间的相互作用,比较了不同方式下主气流氟原子冻结效率及壁面冷却效果。考虑到DF/HF化学激光器主喷管结构尺寸较小,采用适当间隔的单排圆孔注入是现实可行的,并有望达到较好的冷却保护效果,从而提高激光器运转效率。     

迫流冷却二极NbTi超导磁体的研究

首先介绍了导体的测试结果;其次,为评估迫流冷却的二极NbTi超导磁体正常工况下对液氦产生的低温热负荷,基于surf152表面效应单元对线圈盒进行了辐射传热分析;此外,为减小通过线圈盒支撑的传导热负荷并且提高其机械强度,依据线圈盒支撑杆的设计尺寸,提出使用玻璃纤维经过三维编织的各向异性复合材料-G10制作线圈盒支撑杆,从...     

Optimal homotopy asymptotic method with application to thin film flow

A new approximate analytical technique to address for non-linear problems, namely Optimal Homotopy Asymptotic Method (OHAM) is proposed and has been applied to thin film flow of a fourth grade fluid down a vertical cylinder. This approach however, does not depend upon any small/large parameters in comparison to other perturbation method. This method provides a convenient way to control the convergence of approximation series and allows adjustment of convergence regions where necessary. The series solution has been developed and the recurrence relations are given explicitly. The results reveal that the proposed method is very accurate, effective and easy to use.      

用涡方法数值模拟运动物体非定常流场

采用涡方法对静止圆柱绕流、简谐振动圆柱、静止NACA0012翼型绕流和运动扑翼的非定常流场进行了数值模拟和数值验证,对比验证结果较好.控制方程采用二维不可压缩N-S方程,根据算子分裂法,对流和扩散分别采用不同的时间步长.涡方法基于Lagrange坐标系的特点使其方便模拟运动物体的非定常流场.本文的工作为今后的翼型动态失...     

Performance of thermoelectric generator with graphene nanofluid cooling

Improvement of the heat transfer of the cold side is one of the approaches to enhance the performance of TEG systems.As a new type of heat transfer media, nanofluids can enhance the heat transfer performance of working liquid significantly.Based on a three-dimensional and steady-state numerical model,the heat transfer and thermoelectric conversion properties of TEG systems were studied. Graphene anoplatelet aqueous nanofluids were used as the coolants for the cold side of the TEG system to improve the heat transfer capacity of the cold side. The results showed that the heat absorbed by the hot side, voltage, output power, and conversion efficiency of the TEG system were increased greatly by the nanofluid coolants.The output power and the conversion efficiency using 0.1-wt% graphene nanoplatelet aqueous nanofluid as the coolant are enhanced by 26.39% and 14.74%, respectively.     

环形磁场金属等离子体源冷却流场的数值模拟与优化

环形磁场金属等离子体源作为一种全新的等离子体源结构,可用于产生高度离化、无大颗粒、高密度的离子束流,但传统流道结构不能保证其高效、均匀散热,大功率工作时可能引起密封胶圈的烧蚀失效,需对其冷却流场进行优化设计.利用Solidworks Flow Simulation软件对等离子体源冷却流道进行模拟,分析出入水孔分布角度、...     

Wavy film flow down a vertical plate: Comparisons between the results of integral approaches and full-scale computations

This paper is devoted to a theoretical analysis of nonlinear two-dimensional waves using the Navier-Stokes equations in their full statement. Steady-state travelling wave regimes have been found and an analysis of their linear stability has been carried out. It is shown that the flow regimes obtained using the Navier-Stokes equations are qualitatively different from the solutions of Shkadov’s integral approach starting from some values of the Kapitza number. It is also found that the wave regimes of the Navier-Stokes equations have an internal vortex at moderate Reynolds numbers. The results obtained using “the regularized integral model” are in excellent agreement with the Navier-Stokes calculations for Re/Ka ≤2. Unlike the solutions found using an integral approach, it is shown that only a few types of nonlinear waves exist when the full Navier-Stokes equations are considered. The text was submitted by the author in English.     

Transient thin film flow of nonlinear radiative Maxwell nanofluid over a rotating disk

In this letter, a mathematical model for transient nature thin film flow of Maxwell nanofluid over a rotating disk is studied in the presence of a uniform magnetic field and non-linear thermal radiation. The Brownian motion and thermophoresis features due to nanofluid are captured by adopting the Buongiorno model. The prime emphasize is to explore the temperature field and nanoparticles volume fraction in nanofluid thin film flow. The reduced system of differential equations is solved numerically by finite difference based method namely bvp4c. The numerical outcomes regarding film thickness, Nusselt number, Sherwood number, velocity, temperature, and concentration are revealed for varying estimation of involved physical parameters. It is shown that the film thickness decreases with increasing values of the magnetic number. Further, the impact of thermophoresis and thermal radiation parameters is worthwhile in enhancing the fluid temperature. The Solute concentration is found to decrease with Brownian motion and Schmidt number.     

液滴撞击液膜的射流与水花形成机理分析

建立了单液滴撞击平面液膜的物理与数学模型,采用Coupled Level Set and Volume of Fluid方法对这种现象进行了数值模拟,探讨了黏度和表面张力对冠状水花形态的影响.通过分析撞击后液体内部的压力和速度分布,揭示了液滴颈部射流的产生机理,验证了Yarin和Weiss提出的运动间断理论.研究显示,表面张力对冠状水花形态的影响远大于黏度的影响.颈部射流的产生主要是由于撞击后颈部区域局部较大压差造成的,随着撞击过程的继续,压差作用减弱;液膜内流体的径向运动对射流发展成冠状水花具有推动作用.     

水平磁场中液态锂膜流动实验装置及初步结果

设计了用于水平磁场中锂膜流动铺展性及磁流体动力学效应研究的实验装置，介绍了所用磁铁、锂循环回路、动力系统、回路温控系统和测量系统五个组成部分。各部分加工完成，进行现场组装与回路调试，最后加入锂锭熔融后完成实验台搭建工作。利用该实验台研究了锂膜在不锈钢表面的铺展情况、锂膜表面形态与流动雷诺数的关系，以及磁场对液膜表面形态的影响等方面。结果发现液态锂膜在充分锂浸润的不锈钢表面能够完全铺展，水平磁场对锂膜流动有致稳作用，并且可以抑制磁场方向的表面波动。     

Numerical Analysis of Unsteady Magneto-Biphase Williamson Fluid Flow with Time Dependent Magnetic Field

Numerical investigation of the dusty Williamson fluid with the dependency of time has been done in current disquisition. The flow of multiphase liquid/particle suspension saturating the medium is caused by stretching of porous surface. The influence of magnetic field and heat generation/absorption is observed. It is assumed that particle has a spherical shape and distributed uniformly in fluid matrix. The unsteady two-dimensional problems are modeled for both fluid and particle phase using conservation of mass, momentum and heat transfer. The finalized model generates the non-dimensioned parameters, namely Weissenberg number, unsteadiness parameter, magnetic parameter,heat generation/absorption parameter, Prandtl number, fluid particle interaction parameter, and mass concentration parameters. The numerical solution is obtained. Locality of skin friction and Nusselt number is deliberately focused to help of tables and graphs. While inferencing the current article it is clearly observed that increment of Williamson parameter, unsteadiness parameter, magnetic parameter, volume fraction parameter, and mass concentration parameter reduces the velocity profile of fluid and solid particles as well. And increment of Prandtl number, unsteadiness parameter,volume fraction parameter, and mass concentration parameter reduces the temperature profile of fluid and solid particles as well.     

Numerical investigation of laminar flow and heat transfer in a radial flow cooling system with the use of nanofluids

Nanofluids, because of their enhanced heat transfer capability as compared to normal water/glycol/oil based fluids, offer the engineer opportunities for development in areas where high heat transfer, low temperature tolerance and small component size are required. In this present paper, the hydrodynamic and thermal fields of a water–γAl₂O₃ nanofluid in a radial laminar flow cooling system are considered. Results indicate that considerable heat transfer enhancement is possible, even achieving a twofold increase in the case of a 10% nanoparticle volume fraction nanofluid. On the other hand, an increase in wall shear stress is also noticed with an increase in particle volume concentration.     

TiAl合金薄膜在冷却过程中结构变化的原子尺度计算研究

采用基于嵌入原子势模型的分子动力学方法模拟了熔融TiAl合金薄膜分别在急冷降温和连续降温两个冷却过程中微观结构的变化.通过应用原子平均能量、对分布函数和键对分析技术等对薄膜内原子局域结构进行的分析. 研究表明,在降温过程中,薄膜内局域结构出现分阶段变化的特点.在急冷降温过程中,薄膜结构的变化可以分为3个阶段,而在连续降温过程中,薄膜内局域结构的变化分为2个阶段. 关键词： 分子动力学 TiAl合金 薄膜 计算机模拟     

Experimental and numerical study of the effect of conjugate heat transfer on film cooling

Combined convection heat transfer and thermal conduction for film cooling of a flat plate with 45° ribs on one wall was investigated experimentally and numerically. The flat plate surface temperature was measured using thermochromic liquid crystals. The results show that the film cooling is the main mechanism for the local cooling with a very low thermal conductivity while the convection heat transfer of the coolant in the coolant channel is the dominant heat transfer mechanism for the high thermal conductivity plate, with both film cooling and convection heat transfer by the coolant being important with medium thermal conductivity walls.     

涡轮叶片端壁槽缝气与离散气膜孔冷却特性实验研究

真实发动机涡轮叶片端壁为曲面造型,并且其冷却受槽缝气、泄漏流和离散气膜冷却多种冷却气叠加影响,同时又受到主流二次流影响,因此呈现复杂冷却特性。为研究接近真实发动机涡轮叶片端壁构型和工况下的气膜冷却特性,本文采用高速风洞(主流雷诺数为37万)及压敏漆(PSP)技术,研究了槽缝气、泄漏流以及离散气膜对曲面端壁的气膜冷却效率的影响,并针对不同冷气流量比对端壁气膜冷效的影响规律进行了对比分析。结果表明:端壁表面气膜冷效随着槽缝气流量比增大而增大,当流量比增大到1.71%时,槽缝气膜几乎可以覆盖整个端壁表面;与槽缝气相比,端壁表面的离散气膜冷气覆盖范围较为有限,端壁压力面侧下游区域气膜覆盖较差;在喉部之前,随着流量比增大,离散气膜冷效呈现下降趋势;在喉部之后,随着流量比从1.3%增大到1.9%,离散气膜冷效呈现上升趋势;与仅有离散气膜相比,包含槽缝气、泄漏流、离散气膜的全气膜覆盖更为均匀,全气膜冷效的叠加使得端壁冷效相比仅有离散气膜时整体提高了93.4%。