PVM平台下三维超声速钝头体底部流场的并行数值模拟及其拓扑分析

用拼接法划分网格，并运用基于消息传递的并行软件平台ＰＶＭ分配计算任务，实现了较大规模的三维超声速钝头体底部流场的并行数值模拟。结果表明，底部压强特性与实验符合较好，流场的拓扑结构合理。     

逃逸飞行器喷流干扰流场的分区数值模拟

基于拼接网格系统 ,应用三维区域边界格式 ;通过区域边界格式对区域边界上的通量进行守恒性处理 ,发展了一个超音速复杂流场分区算法 ;对不同攻角下的逃逸飞行器喷流干扰流场进行了分区数值模拟 ,取得了较好的结果     

简单离心喷油器的试验研究(Ⅰ)——理论公式的误差分析

本文以试验台冷态试验为基础,以实际喷油器为对象,通过大量试验资料对阿勃拉莫维奇理论公式的误差分布与误差原因进行了分析。从大量试验资料中归纳出一个决定流量系数比值μ/μ_A变化规律的组合几何尺寸Z_w,而判别式R_z/R_(Qd)(?)d_p更进一步揭示了它与μ_z/μ_A1.0之间的内在联系。文章还详细分析了雾化片中的流动阻力及其决定因素,最后以充分的数据找到并论证了理论公式产生误差的真正原因在于雾化片本身的几何特性数A,由此提出了减小设计误差的方法——雾化片几何尺寸的最佳流动组合。     

二元翼型跨音速非定常测压实验研究

本文描述了在南航ＮＨ－１风洞中,对ＮＡＣＡ００１２翼型绕其１／４弦长处轴作俯仰正弦振动时,跨音速非定常压力测量的实验。实验目的在于研究在跨音速风洞中二元翼型非定常压力实验中的技术问题,包括实验装置的设计,数据采集和处理等,并初步研究了Ｍ数、攻角、振幅等参数对非定常压力分布的影响。     

热式流量传感器辨识与数字补偿方法

本文就改善热式流量传感器的响应特性问题进行了理论与实验研究,指出了模拟电路补偿方法所存在的不足,论述了热式流量传感器的辨识与实验方法,提出了用数字补偿提高其响应速度的方法。研究表明,这种方法是很有效的。     

激励器结构参数对合成射流影响的试验研究

为了设计高性能的合成射流激励器,实验采用热线风速仪测量激励器出口的流动速度,对不同大小激励器、不同出口形状激励器、单 双膜激励器以及金属振动膜处于不同装配受压状态下的激励器分别进行了试验。实验结果显示:激励器的结构决定了合成射流激励器的性能;激励器出口射流平均速度除了与激励器大小、出口面积有关外,还与出口形状有关,采用方孔 矩形孔形式的开口有利于建立较强的合成射流;双膜与单膜工作相比,合成射流最大速度基本上是成两倍关系;金属振动膜的安装形式(受压状态)不影响合成射流随频率的变化规律,但对合成射流速度影响很大,当激励器振动膜处于螺栓拧紧受压状态时,与振动膜不受压状态相比,合成射流出口速度几乎下降了一个数量级。     

数组越界软件测试系统的设计与实现

软件测试系统的研制是现阶段软件测试领域研究的一个热点.首先针对C/C 语言常见数组越界错误类型进行了分析,介绍了软件测试的一些基本概念,而后给出了软件测试系统设计,对系统设计的各个阶段进行了说明,并且给出了一种错误类型检查的算法设计,它在软件测试检测中具有通用性和代表性,最后给出了软件测试的实验结果.     

Numerical studies on four-engine rocket exhaust plume impinging on flame deflectors with afterburning

This paper studies the four-engine liquid rocket flow field during the launching phase. Using three-dimensional compressible Navier-Stokes equations and two-equation realizable k-epsilon turbulence model, an impact model is established and flow fields of plume impinging on the two different shapes of flame deflectors, including wedge-shaped flame deflector and cone-shaped flame deflector, are calcu-lated. The finite-rate chemical kinetics is used to track chemical reactions. The simulation results show that afterburning mainly occurs in the mixed layer. And the region of peak pressure occurs directly under the rocket nozzle, which is the result of the direct impact of exhaust plume. Compared with the wedge-shaped flame deflector, the cone-shaped flame deflector has great performance on guiding exhaust gas. The wedge-shaped and cone-shaped flame deflectors guide the supersonic exhaust plume away from the impingement point with two directions and circumferential direction, respectively. The maximum pressure and temperature on the wedge-shaped flame deflector surface are 37.2% and 9.9% higher than those for the cone-shaped flame deflector. The results provide engineering guidance and theoretical significance for design in flame deflector of the launch platforms.     

Numerical research on adverse effect of muzzle flow formed by muzzle brake considering secondary combustion

The simulation of the artillery interior and intermediate ballistics problem is performed to investigate the influence of a gas dynamics device, muzzle brake, on the muzzle hazard phenomena, such as flash and blast waves. The correlation of the chemical reactions with the characteristics of the muzzle flow field is analyzed by the simulation for a further understanding of the secondary combustion phenom-enon of the muzzle flow. The novel structure of muzzle flow caused by the muzzle brake is presented by the simultaneous solution of the interior ballistics model and multi-species Navier-Stokes equations in order to analyze the influence of the muzzle brake structure on the chemical reactions. The secondary combustion of the muzzle flow due to the oxygen-supplement chemical reactions is obtained by the chemical reaction kinetic model. The interaction of the blast waves released from the muzzle brake is illustrated in detail and the mechanism of the formation of muzzle flash is analyzed. This research provides a reference for the studies on the suppression of the muzzle flash.     

On the asymptotic optimality of algorithms for the flow shop problem with release dates

We consider the nonpermutation flow shop problem with release dates, with the objective of minimizing the sum of the weighted completion times on the final machine. Since the problem is NP‐hard, we focus on the analysis of the performance of several approximation algorithms, all of which are related to the classical Weighted Shortest Processing Time Among Available Jobs heuristic. In particular, we perform a probabilistic analysis and prove that two online heuristics and one offline heuristic are asymptotically optimal. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005.