COMPUTATION OF SUPERSONIC TURBULENT FLOWFIELD WITH TRANSVERSE INJECTION

ＩｎｔｒｏｄｕｃｔｉｏｎＴｈｅｍｉｘｉｎｇｆｌｏｗｆｉｅｌｄｒｅｓｕｌｔｉｎｇｆｒｏｍａｓｏｎｉｃｇａｓｅｏｕｓｉｎｊｅｃｔｉｏｎｉｎｊｅｃｔｅｄｔｒａｎｓｖｅｒｓｅｌｙｉｎｔｏａｓｕｐｅｒｓｏｎｉｃｆｒｅｅｓｔｒｅａｍｉｓｅｎｃｏｕｎｔｅｒｅｄｉｎｍａｎｙｆｉｅｌｄｓｓｕｃｈａｓｒｏｃｋｅｔｍｏｔｏｒｔｈｒｕｓｔｖｅｃｔｏｒｃｏｎｔｒｏｌｓｙｓｔｅｍｓ,ｓｕｐｅｒｓｏｎｉｃｃｏｍｂｕｓｔｉｏｎ ,ｈｉｇｈ＿ｓｐｅｅｄｆｌｉｇｈｔｖｅｈｉｃｌｅｒｅａｃｔｉｏｎｃｏｎｔｒｏｌｊｅｔｓ,ａｎｄｇａｓ＿ｔ…     

带用横向射流的三维超声速湍流流场分析

应用显式的五阶WENO格式，结合k-ω湍流模型，求解三维Favre平均N－S方程，计算了从方孔横向喷出的声速气流与马赫数为3．0的超声速气流的干扰流场。结果表明，在射流上游，射流的阻碍便超声速气流产生分离，形成两个主要的回流区域，主回流导致在方孔射流两侧形成马蹄涡区域，射流下游存在低压区域，形成较小的回流以及一对螺流形旋涡。     

不同气体工质对激光推力器冲量耦合系数的影响

通过冲击摆实验,测量了激光推力器在不同气体工质(氩气,氦气)、不同工作压力条件下的冲量耦合系数,比较了不同气体对激光推力器冲量耦合系数的影响.实验结果表明:冲量耦合系数随着环境压力的下降而下降,并且下降趋势越来越快;在氩气中测量的冲量耦合系数比氦气的高;实验产生误差的主要因素是摆角的测量误差.     

密相液固两相湍流K-ε-T模型及其在管道两相流中的应用

为了准确预测密相液固两相湍流流动,建立了Ｋ－ε－Ｔ模型,推导了控制方程组。利用该模型对竖直上升管中的密相液固两相流动进行了数值模拟,得到了与实验值吻合较好的结果。     

K-ε-T MODEL OF DENSE LIQUID-SOLID TWO-PHASE TURBULENT FLOW AND ITS APPLICATION TO THE PIPE FLOW

ＩｎｔｒｏｄｕｃｔｉｏｎＬｉｑｕｉｄ＿ｓｏｌｉｄｔｗｏ＿ｐｈａｓｅｆｌｏｗｅｘｉｓｔｓｗｉｄｅｌｙｉｎｎａｔｕｒｅａｎｄｍａｎｙｉｎｄｕｓｔｒｉａｌｍｉｎｉｓｔｒｉｅｓ,ｆｏｒｅｘａｍｐｌｅ,ｓｅｄｉｍｅｎｔ＿ｌａｄｅｎｗａｔｅｒｆｌｏｗｉｓａｃｈａｒａｃｔｅｒｉｓｔｉｃｌｉｑｕｉｄ＿ｓｏｌｉｄｔｗｏ＿ｐｈａｓｅｆｌｏｗｉｎｎａｔｕｒｅａｎｄｈｙｄｒａｕｌｉｃｔｒａｎｓｐｏｒｔｏｆｓｏｌｉｄｍａｔｅｒｉａｌｉｓａｃｈａｒａｃｔｅｒｉｓｔｉｃｉｎｄｕｓｔｒｉａｌａｐｐｌｉｃａｔｉｏｎ.Ｔｈｅｓｔｕｄ…     

宾汉流体物性参数对湍流强度影响的研究

考虑宾汉流体本构关系的特点，建立了适用于宾汉流体的修正动量方程和Ｋτ－ετ模型方程。采用压力耦合半隐式ＳＩＭＰＬＥ算法，通过流场的数值计算研究，指出了宾汉流体本身的物性参数（如屈服应力、塑性粘度）对其湍流强度有着重要影响。     

DROPLET COLLISION AND COALESCENCE MODEL

A new droplet collision and coalescence model was presented,a quick-sort method for locating collision partners was also devised and based on theoretical and experimental results,further advancement was made to the droplet collision outcome. The advantages of the two implementations of smoothed particle hydrodynamics (SPH) method were used to limit the collision of droplets to a given number of nearest droplets and define the probability of coalescence,numerical simulations were carried out for model validation.Results show that the model presented is mesh-independent and less time consuming,it can not only maintains the system momentum conservation perfectly,but not susceptible to initial droplet size distribution as well.     

EFFECT OF EMPIRICAL COEFFICIENTS ON SIMULATION IN TWO-SCALE SECOND-ORDER MOMENT PARTICLE-PHASE TURBULENCE MODEL

A two-scale second-order moment two-phase turbulence model accounting for inter-particle collision is developed, based on the concept of particle large-scale fluctuation due to turbulence and particle small-scale fluctuation due to collision. The proposed model is used to simulate gas-particle downer reactor flows. The computational results of both particle volume fraction and mean velocity are in agreement with the experimental results. After analyzing effects of empirical coefficient on prediction results, we can come to a conclusion that, inside the limit range of empirical coefficient, the predictions do not reveal a large sensitivity to the empirical coefficient in the downer reactor, but a relatively great change of the constants has important effect on the prediction.     

DIFFERENCE SCHEME FOR TWO-PHASE FLOW

A numerical method for two-phase flow with hydrodynamics behavior was considered. The nonconservative hyperbolic governing equations proposed by Saurel and Gallout were adopted. Dissipative effects were neglected but they could be included in the model without major difficulties. Based on the opinion proposed by Abgrall that “a two phase system, uniform in velocity and pressure at t = 0 will be uniform on the same variable during its temporal evolution“, a simple accurate and fully Eulerian numerical method was presented for the simulation of multiphase compressible flows in hydrodynamic regime. The numerical method relies on Godunov-typescheme, with HLLC and Lax-Friedrichs type approximate Riemann solvers for the resolution of conservation equations, and nonconservative equation. Speed relaxation and pressure relaxation processes were introduced to account for the interaction between the phases. Test problem was presented in one space dimension which illustrated that our scheme is accurate, stable and oscillation free.     

三氧化二铝液滴对心碰撞直接数值模拟

为研究固体火箭发动机内三氧化二铝液滴碰撞的物理规律及结果预测模型,针对两个相同尺寸的三氧化二铝液滴对心碰撞,开展了直接数值模拟.首先进行了正十四烷液滴在氮气环境下的对心碰撞数值研究,数值与实验结果基本一致,验证了计算方法的可行性及准确性.针对三氧化二铝液滴开展了6 MPa压强下不同Weber数的对心碰撞数值研究,计算Weber数范围为10~200,Ohnesorge数为0.036 4;获得了反弹、大变形后聚合和自反分离3种结果类型,反弹与大变形后聚合的临界分离Weber数为26,大变形后聚合与自反分离的临界分离Weber数为44.根据临界Weber数对其他流体液滴碰撞模型进行修正,可以获得三氧化二铝液滴的碰撞模型.