12150L发动机系统工作过程计算

介绍了12150L发动机系统工作过程模拟计算方法的研究成果,包括发动机燃烧、喷油、进排气和废气引射抽尘过程的数学建模,耦合计算等.     

高空滑移条件对化学非平衡粘性流动的影响

本文用数值方法计算了不同高度滑移边界条件对钝体绕流流场特性的影响。采用化学非平衡粘性激波层控制方程,边界条件含壁面滑移、激波滑移和无滑移条件。计算结果表明,考虑滑移条件后,激波层较厚,激波处的电子数密度为一有限值。文中给出了计算结果,并与其它文献的结果作了比较。     

旋转稳定塑料弹体工程设计计算研究

本文以实验结果为依据,首先分析了塑料弹体影响弹丸膛内运动的物理性能,然后结合旋转弹丸的膛内运动特征,经过模拟试验,采用数学拟合法,初步建立旋转稳定弹塑料弹体工程设计计算的数学模型(包括结构尺寸设计计算、强度计算和内弹道计算)。     

基于Matlab的线性拟合计算

对于弹道导弹,由于其运动受多种因素的影响,因此描述其运动的微分方程是极其复杂的,而且,方程中的部分参数是通过对试验数据的科学处理获得的.为了建立数学模型,有时用数据拟合的方法对试验数据进行处理.运用单变量、多变量的线性拟和方法,给出了"单输入/单输出"、"多输入/单输出"的线性拟合模型,并针对拟合模型中未知参数的确定问题,给出了基于最小二乘的线性矛盾方程组的求解方法.通过仿真计算,能够得到较高精度的计算结果.最后,给出了Matlab的实现方法,并给出了一段具体的实现程序.     

挠度对钢丝绳弹性模量的影响

钢丝绳被广泛地应用在油气储运工程中。弹性模量是钢丝绳的一个重要物性参数,欧洲和前苏联对该问题研究较多,他们用实验的方法得到钢丝绳弹性模量的经验计算公式。笔者引用等效弹性模量的概念,根据悬索的斜抛物线长度计算公式,从理论上推导了挠度对钢丝绳弹性模量影响的计算公式。该公式推导过程简单,且可以定量地计算挠度对钢丝绳弹性模量的影响。     

舰炮对岸无瞄准点射击诸元计算模型

介绍了一种新的舰炮射击方法--舰炮对岸无瞄准点射击概念、原理,建立了目标相对坐标计算模型、观测舰位坐标转换模型,解决了水面舰艇舰炮对岸上目标射击诸元计算问题.舰炮对岸无瞄准点射击,解决了水面舰艇全天候对岸应召射击问题,显著提高了舰炮对岸打击能力和战术使用的灵活性.     

船载炮对岸射击的特点及射击诸元计算

根据陆炮的结构性能和使用特点,对陆炮在射击平台由陆地改变为舰船时,对岸射击的特点、非标准弹道气象条件对射击的影响及修正、目标高低角及高角差的影响和修正、摇摆的影响及措施等进行了研究与分析。解决了船载炮射击时射击诸元计算与射击条件相适应的问题,并具体分析了船载炮对岸射击时射击诸元计算的原理公式、计算方法和实施方法。     

基于动态模型的机场配电网潮流计算新方法

机场配电网因非常情况成为孤立电力系统后,配电系统的电压、潮流和频率等发生巨大变化,传统的潮流计算方法往往会出现收敛性差、计算结果与实际不相符的情况。提出的机场配电网动态潮流计算模型能有效解决此类问题,阐述了机场配电网动态潮流计算模型的构成原理、算法并给出相应算例。通过算例计算证明了动态潮流计算模型适用于计算机场配电网的潮流。     

Modeling of the whole process of shock wave overpressure of free-field air explosion

The waveform of the explosion shock wave under free-field air explosion is an extremely complex problem. It is generally considered that the waveform consists of overpressure peak, positive pressure zone and negative pressure zone. Most of current practice usually considers only the positive pressure. Many empirical relations are available to predict overpressure peak, the positive pressure action time and pressure decay law. However, there are few models that can predict the whole waveform. The whole process of explosion shock wave overpressure, which was expressed as the product of the three factor functions of peak, attenuation and oscillation, was proposed in the present work. According to the principle of explosion similarity, the scaled parameters were introduced and the empirical formula was absorbed to form a mathematical model of shock wave overpressure. Parametric numerical simulations of free-field air explosions were conducted. By experimental verification of the AUTODYN numerical method and comparing the analytical and simulated curves, the model is proved to be accurate to calculate the shock wave overpressure under free-field air explosion. In addition, through the model the shock wave overpressure at different time and distance can be displayed in three dimensions. The model makes the time needed for theoretical calculation much less than that for numerical simulation.     

Effect of tongue clearance on hydraulic performance of double support vortex pump

In order to study influence of tongue clearance on the hydraulic performance of double support vortex pump, three dimensional flow model with symmetric variable size tongue clearance was established by changing section parameter of tongue clearance, and applied to numerically simulate the steady inner flow in a vortex pump based on fixed working conditions and impeller through ANSYS FLUENT. The numerical results show the influence of tongue channel with two sections (non-uniform and uniform sections) on flow field characteristics in vortex pump. Firstly, the variation of tongue channel section changes the vortex structure distribution in circumferential flow channel. Specifically the spiral forward vortex structure in the circumferential direction shifts to large radius side with increasing tongue width. Secondly, the circumferential velocity gradient and axial pressure gradient both diminish with the increase of the tongue section, and the inlet/outlet pressure difference and velocity distribution also reduce with increasing tongue channel section. Finally, for vortex pump with non-uniform section of tongue channel, the head diminishes and the efficiency remains constant approximately with the increase of the tongue width, while the head and the efficiency both diminish for uniform section of tongue channel.