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某飞行器空气流体动力参数计算与弹道仿真 被引量:2
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作者 康宝臣 郭志军 冯丽娜 《兵工自动化》 2019年第2期29-34,共6页
为了有效指导飞行器结构设计,获得风洞试验不能获得的中间参数,减少风洞试验的次数,在现有仿真文献优点的基础上,运用Pro/Engineer、ANSA、Fluent和Matlab等软件对某飞行器的几何外形、非结构流体网格划分、流体动力参数和无动力飞行弹... 为了有效指导飞行器结构设计,获得风洞试验不能获得的中间参数,减少风洞试验的次数,在现有仿真文献优点的基础上,运用Pro/Engineer、ANSA、Fluent和Matlab等软件对某飞行器的几何外形、非结构流体网格划分、流体动力参数和无动力飞行弹道数据进行处理和计算。通过MPI并行计算和JOU批处理自编程序,完成96种工况千万级网格数量下的流体动力参数高精度计算,运用Matlab自编程序结合经典四阶龙格库塔法和拉格朗日插值算法求解飞行器纵向运动方程组完成空中飞行弹道仿真。结果表明:该仿真结果能有效指导某飞行器结构设计,减少风洞试验次数,获得风洞试验不能获得的中间参数,缩短研制周期,节约研制经费。 展开更多
关键词 流体动力参数 转动惯量 高精度计算 弹道仿真
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Effects of expanding zone parameters of vacuum dust suction mouth on flow simulation results 被引量:9
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作者 章易程 杨春朝 +3 位作者 Chris Baker 陈默 邹翔 戴万林 《Journal of Central South University》 SCIE EI CAS 2014年第6期2547-2552,共6页
Based on the parametric analysis of the expanding zone of the vacuum dust suction mouth,the flow in the vacuum dust suction mouth was simulated by computational fluid dynamics(CFD)software,Fluent.The effects of the ex... Based on the parametric analysis of the expanding zone of the vacuum dust suction mouth,the flow in the vacuum dust suction mouth was simulated by computational fluid dynamics(CFD)software,Fluent.The effects of the expanding zone parameters on flow simulation were analyzed.The results show that simulation effects depend on threshold values of the expanding zone parameters of the dust suction mouth,and the threshold values of the expanding zone can be obtained according to the different structures of the vacuum dust suction mouth and be selected as the geometric parameters in calculating,and also corners of the expanding zone make unobvious difference in calculation accuracy and in computational efficiency compared with no corner.The simulation results provide practical guidance to the flow simulation on the dust suction mouth. 展开更多
关键词 dust suction mouth expanding zone threshold analysis computational fluid dynamics
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Numerical simulation of effect of bionic V-riblet non-smooth surface on tire anti-hydroplaning 被引量:4
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作者 周海超 王国林 +1 位作者 杨建 薛开鑫 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第10期3900-3908,共9页
Inspired by the idea that bionic non-smooth surfaces(BNSS) can reduce fluid adhesion and resistance, and the effect of bionic V-riblet non-smooth structure arranged in tire tread pattern grooves surface on anti-hydrop... Inspired by the idea that bionic non-smooth surfaces(BNSS) can reduce fluid adhesion and resistance, and the effect of bionic V-riblet non-smooth structure arranged in tire tread pattern grooves surface on anti-hydroplaning performance was investigated by using computational fluid dynamics(CFD). The physical model of the object(model of V-riblet surface distribution, hydroplaning model) and SST k-ω turbulence model were established for numerical analysis of tire hydroplaning. With the help of a orthogonal table L16(45), the parameters of V-riblet structure design compared to the smooth structure were analyzed, and obtained the priority level of the experimental factors as well as the best combination within the scope of the experiment. The simulation results show that V-riblet structure can reduce water flow resistance by disturbing the eddy movement in boundary layers. Then, the preferred type of V-riblet non-smooth structure was arranged on the bottom of tire grooves for hydroplaning performance analysis. The results show that bionic V-riblet non-smooth structure can effectively increase hydroplaning velocity and improve tire anti-hydroplaning performance. Bionic design of tire tread pattern grooves is a good way to promote anti-hydroplaning performance without increasing additional groove space, so that tire grip performance and roll noise are avoided due to grooves space enlargement. 展开更多
关键词 TIRE anti-hydroplaning bionic non-smooth surfaces(BNSS) numerical simulation
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