高超声速飞行器两类典型防热材料的性能表征与评价

针对高超声速飞行器翼前缘用超高温陶瓷材料及机身大面积金属热防护结构材料在高温环境下的力学响应分析与评价方法进行了全面的回顾和总结.综述了大面积金属热防护系统在传热、静力学、热力耦合性能、疲劳性能及抗冲击性能等方面国内外的研究进展;以及超高温陶瓷材料在热冲击、增韧机制、抗氧化性能等方面评价与表征技术,并结合国内研究状况展望了今后的发展方向.      

基于神经网络技术的乘波体优化设计

乘波体是高超声速飞行器的主要组成部分,也是飞行器产生升力的主要部分. 针对基 于计算流体动力学(CFD)分析的乘波体优化设计问题,引入人工神经元网络响应面方法. 选 取一定数量的乘波体外形,进行气动性能分析后,利用乘波体的外形控制参数和气动参数做 为训练样本对乘波体进行训练. 利用这些训练样本对人工神经网络进行训练. 在优化计算中 以充分训练的神经网络替代CFD分析,发展了一种基于神经网络技术的乘波体优化设计方法. 利用该方法在马赫数6、雷诺数7\times 10^6条件下,分别对乘波体进行了最大升阻比的单目标和综 合考虑升阻比、容积及表面积的多目标优化. 计算结果表明,采用神经网络响应面技术可在 保证计算稳定性的条件下有效提高计算效率.     

Research progress on thermal protection materials and structures of hypersonic vehicles

Hypersonic vehicles represent future trends of military equipments and play an important role in future war. Thermal protection materials and structures, Which relate to the safety of hypersonic vehicles, are one of the most key techniques in design and manufacture of hypersonic vehicles. Among these materials and Structures, such as metallic temperature protection structure, the temperature ceramics and carbon/carbon composites are usually adopted in design. The recent progresses of research and applica- tion of ultra-high temperature materials in preparation, oxidation resistance, mechanical and physical characterization are summarized.     

高温真实气体底部流动的NS方程数值计算

本文数值模拟了高超音速飞行时钝锥的底部流动。采用轴对称NS方程并考虑真实气体效应。湍流模型采用修正的Baldwin-Lomax涡粘性代数模型,数值方法空间离散对流项采用显式NND格式,粘性项采用中心差。时间离散采用三阶的龙格-库塔法。真实气体模型采用考虑七种组分四种反应的汉森模型。给出了底部流场的压力和温度分布及各组分的浓度分布。可以看出在近底部区域高速流-绕过拐角就产生一回流旋涡区。由于温度变化很大,气体的热力学特性受气体离解、复合和振动能激发的影响。所以整个流动过程变得十分复杂。     

Initiation Efficiency Reduction in Semicontinuous Styrene and Butyl Acrylate Emulsion Copolymerization Reactions

The decrease of initiation efficiency (radical entry efficiency) during seeded emulsion copolymerizations of styrene and butyl acrylate with different residual monomer reduction strategies was evaluated. Experiments were carried out using 50 and 99wt.% of styrene in monomer feed stream. Simulations were performed with a detailed mathematical model of the process that takes into account the diffusion control of initiation, propagation and termination. Results showed that the radical entry into polymer particles is strongly influenced by the aqueous phase kinetics and by the monomer solubility in aqueous phase. Simulation results were compared to experimental results of residual monomer and showed that the residual monomer content can be reduced by a temperature increase at the end of the polymerization. However, an additional feeding of more initiator, even when combined with such an increase of temperature, did not lead to a smaller residual monomer content due, mainly, the kinetic of termination in aqueous phase and radical anchoring. A model that accounts for the reduction of initiator efficiency (free radical entry efficiency) was successfully used to explain the behavior of the experimental observations and was able to correctly predict the qualitative trends of the effectiveness of different residual monomer reduction strategies.     

Forebody compressibility research of hypersonic vehicle

IntroductionTheintegrateddesignofairframe propulsionofhypersonicvehicleisoneofthekeytechnologyfortheair_breathingenginehypersonicvehicles[1～4 ].Thepurposestodointegrateddesignofforebody inletaretoputtheforebodyasthepre_compressiveramp ,toprovideuniformflowfield ,whichmeanssmallpressureandvelocitygradient,smallorientalangleofgasflowandlowaverageMachnumberattheentryoftheinlet,andenoughfluxfortheinlet,furthermoretomeetthedesignrequestofinlet.Ontheotherhand ,itmustbenon_sensitivetotheMachnumbera…     

高超声速平板边界层流动显示的试验研究

本文在高超声速脉冲式风洞内对基于纳米示踪的平面激光散射技术(nano-based planar laser scattering, NPLS)的应用进行了探索, 并在此基础上对平板边界层流动结构的精细测量进行了研究. 试验来流Ma=7.3, 总压4.8 MPa, 总温680 K. 通过时序的分析和调试, 对各分系统实现了高精度的同步控制; 定量的粒子注入及混合, 实现了粒子的均匀撒播, 对主流获得了均匀的显示效果; 对于边界层流动, 获得了精细的瞬态流动结构图像, 显示了层流到湍流的转捩过程, 并分析了其时空演化特性.     

A hybrid DSMC/Navier–Stokes frame to solve mixed rarefied/nonrarefied hypersonic flows over nano‐plate and micro‐cylinder

We extend a hybrid DSMC/Navier–Stokes (NS) approach to unify the DSMC and the NS simulators in one framework capable of solving the mixed non‐equilibrium and near‐equilibrium flow regions efficiently. Furthermore, we use a one‐way state‐based coupling (Dirichlet–Dirichlet boundary‐condition coupling) to transfer the required information from the continuum region to the rarefied one. The current hybrid DSMC–NS frame is applied to the hypersonic flows over nanoflat plate and microcylinder cases. The achieved solutions are compared with the pure DSMC and NS solutions. The results show that the current hybrid approach predicts the surface heat transfer rate and shear stress magnitudes very accurately. Some important conclusions can be drawn from this study. For example, although the shock wave region would be a non‐equilibrium region, it is not necessary to use a pure DSMC simulator to solve it entirely. This is important when the researchers wish to predict the surface properties such as velocity slip, temperature jump, wall heat flux rate, and friction drag magnitudes accurately. Our investigation showed that our hybrid solution time would be at least 40% (for the flat plate) and 35% (for the cylinder) of the time that must be spent by a pure DSMC solver to attain the same accuracy.Copyright © 2013 John Wiley & Sons, Ltd.     

Simulation of two‐phase flow–body interaction problems using direct forcing/fictitious domain–level set method

In the present paper, a direct forcing/fictitious domain (DF/FD)–level set method is proposed to simulate the twophase flow–body interaction. The DF/FD does not sacrifice accuracy and robustness by employing a discrete δ (Dirac delta) function to transfer quantities between the Eulerian nodes and Lagrangian points explicitly as the immersed boundary method. The advantages of this approach are the simple concept, the easy implementation and the utilization of original governing equation without modification. The main idea is to combine DF/FD method with the level set method in the Cartesian coordinates. We present the results of a number of test cases to illustrate the effectiveness of the proposed method for single‐phase flow–body interaction problem and the two‐phase flows with a stationary body. Eventually, the simulations of various water entry problems have been conducted to validate the capability and the accuracy of the present method on solving the twophase flow–body interaction. Consequently, the present results are found to be in good agreement with those of previous studies. Copyright © 2013 John Wiley & Sons, Ltd.     

ENTRY AND EXIT OF LABOR AND CAPITAL IN A FISHERY

ABSTRACT. Exit and entry of fishermen, as well as vessels, is modeled explicitly. If the speed of exit and entry of fishermen is less than instantaneous the wage rate varies with the fortunes of the fishing firms and affects the endogenous labor supply creating a second transmission mechanism from profits to effort. There are realistic cases where this mechanism has important effects on the stability of the dynamic system and on the effects of taxes (subsisdies) on the size of the fish stock. If labor supply depends negatively on the wage rate, the immediate effect of an increase in the tax rate is to increase effort and harvest. This condition makes it also more probable that the dynamic system is unstable. In those cases where the dynamic system is unstable the increase in the tax rate increases overexploitation not only in the short‐term but also in the long‐term.