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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。 相似文献
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IntroductionThemixingflowfieldresultingfromasonicgaseousinjectioninjectedtransverselyintoasupersonicfreestreamisencounteredinmanyfieldssuchasrocketmotorthrustvectorcontrolsystems,supersoniccombustion ,high_speedflightvehiclereactioncontroljets,andgas_t… 相似文献
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在DIPSAR算法的基础上,推导了适用于可压密相气固两相湍流流动数据会计的CDIPSAR算法,利用提出的可压密相的两个k-ε低湍流雷诺数模型,用CDIPSAR算法,对竖直上升管中可压密相气固两相湍流流动进行了数值计算,同时考虑了密度变化和体积分数变化的影响,研究结果表明,随着颗粒体积分数的增加,颗料间及颗粒与壁面间的相互作用占了主导地位,使得单个颗粒脉动速度增大,但是气体及颗粒的速度差却随之减小, 相似文献
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K-ε-T MODEL OF DENSE LIQUID-SOLID TWO-PHASE TURBULENT FLOW AND ITS APPLICATION TO THE PIPE FLOW 总被引:1,自引:0,他引:1
IntroductionLiquid_solidtwo_phaseflowexistswidelyinnatureandmanyindustrialministries,forexample,sediment_ladenwaterflowisacharacteristicliquid_solidtwo_phaseflowinnatureandhydraulictransportofsolidmaterialisacharacteristicindustrialapplication.Thestud… 相似文献
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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. 相似文献
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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。 相似文献
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DROPLET COLLISION AND COALESCENCE MODEL 总被引:3,自引:0,他引:3
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. 相似文献
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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. 相似文献