回转体流噪声相似律的实验研究

介绍了回转体流噪声实验的方法,并对实验测得的回转体流噪声声功率谱的谱特性进行了分析。测量结果表明:在高频段,回转体流噪声声功率谱按6dB/ 倍频程衰减;且其声功率谱与流速的7 次方成正比。基于本实验,验证了回转体流噪声相似律理论     

细长旋成体大迎角绕流非定常特性的实验研究

在亚临界流动范围内,通过细长旋成体在无侧滑状态下的脉动压力测量,对大迎角细长旋成体多涡区域的轴向以及周向的压力脉动特性进行了研究,分析了旋成体周向压力脉动幅度及主频与背涡之间的对应关系,发现在多涡区存在一种完全不同于卡门涡脱落时的非定常现象,得到压力脉动主频的斯特劳哈数沿旋成体轴向有逐渐增大的趋势。     

导弹垂直发射中二次流流场计算

本文应用Ｇｏｄｕｎｏｖ方法对导弹垂直发射系统的内流场进行了数值模拟,详细描述了导弹点火后二次流的形成及其对弹体的影响,为导弹的设计和发射系统的热防护提供参考。     

The structure of Kelvin–Helmholtz vortices with super-sonic flow

We have done two-dimensional simulations of the Kelvin–Helmholtz instability (KHI) with super-sonic flow using the CIP method. The linear analyses of a simple uniform density case show that the KHI cannot grow vigorously when the velocity jump is more than twice the sound speed (when the flow speed relative to the vortex is super-sonic). In this study, by situating a high density contrast across the shear layer, we set the flow in only one of the sides to be super-sonic and then show that the KHI does grow and rolls up a vortex. The formation of a shock is essential for the KHI vigorous growth and the structure of the vortex is strongly influenced by the shock geometry. The results should have substantial implications to velocity shear layer dynamics involving large density jump, such as planetary magnetospheric boundary layers.     

一种典型冲击试验夹具的优化设计

根据冲击试验夹具的设计要求,以夹具几何参数为设计变量,以试件－夹具连接处的期望响应与实际响应差异最小为目标,建立了优化设计的数学模型,同时规定了几何、强度、刚度、体积等约束条件。然后在ANSYS上建立了有限元模型,采用子问题近似方法进行了动力响应优化求解,获得了合理的优化结果。本文的研究为冲击试验夹具的设计提出了一条新思路。