基于Solidworks软件的三维实体建模

介绍了 Solidworks 的特点、建模的基本思路,举例说明了用其进行零件设计、形成装配体和生成二维工程图的过程,并指出了用 Solidworks 所建三维实体模型在虚拟设计和辅助分析中的应用。     

Comparison of various cusp models with high- and low-resolution observations

Three major cusp models are systematically compared with low-resolution (large-scale) and high-resolution (fine-scale) low-altitude observations. Those models are (a) global magnetohydrodynamics (MHD) models (including MHD+drift models), (b) turbulent/diffusive entry models, and (c) direct flowing entry models. Although low-resolution data are mostly consistent with MHD models, high-resolution data mostly contradicts them. The data instead supports the other models in which the cusp is considered as a local `extra' open region. This is a good lesson to us: past supportive `tests' of MHD cusp models might have essential flaws in the methodology, and high-resolution data is necessary even for large-scale modelings.     

超声速分离流非线性湍流模式的研究

本文在低雷诺数k-ε两方程框架下,应用八个常见的非线性湍流模式,对两个激波/边界层相互作用诱导分离的超声速流动进行了研究。采用的非线性模式有:二阶模式(Wilcox＆Rubesin(1980),Shih,Zhu＆Lumley(1993),Shih,Zhu＆Lumley(1995),Gatski＆Speziale(1993))和三阶模式(Craft,Launder＆Suga(1996),Lien＆Leschziner(1996),Apsley＆Leschziner(1998),Shih(1997))。两个超声速流动为:20°可压缩拐角绕流和轴对称尖顶拱-柱-裙组合体绕流。计算结果表明,对于激波边界层相互作用,在不做任何可压缩性修正的情况下,非线性模式并没有给出明显优于线性模式的结果。     

密集模态组间非线性相互作用的初步研究

基于平均 Lagrange函数与调制项关系的 ALFM法,研究了通过 2∶ 1内共振联系的密集模态组间复杂的非线性相互偶合作用,深入探讨了密频内共振与 2∶ 1内共振的关系,提出了密集模态组在低阶主共振条件下相互作用及整体表现的初步规律,对于具有密集模态的大型柔性航空航天结构的振动主动控制和模态分析研究具有重要的指导意义     

Relative ionizations in the nearest interstellar gas

We compare CLOUDY predictions for the equilibrium ionization in the interstellar cloud surrounding the solar system with pick-up ion data. The incident radiation field includes contributions from hot stars, the emission from the conductive cloud boundary and the diffuse FUV back-ground. To within the observational uncertainties, CLOUDY predictions for the ratios n(He)/n(O), n(N)/n(O), n(Ne)/n(O), and n(He)/n(Ne) are consistent with pick-up ion data, provided that O and N are filtered by 50% in the heliopause region and the outer heliosphere as predicted by others. Thus, the steady-state ionization model and assumed radiation field appear approximately valid. However, the youth and low intervening column density towards the Vela pulsar leave open the possibility that the parent supernova explosion 10,500 years ago, and 200 pc distant, may also have affected LISM ionization, although the mechanism is uncertain. Support for this last possibility is provided by the apparent signature of the Vela explosion in the terrestrial geological record.Abbreviations ISM Interstellar Medium - FUV Far Ultraviolet - EUV Extreme Ultraviolet - SNR SN remnant - SXRB SXR Background - LISM Local Interstellar Matter     

试验有限元建模和模型修改

 CATAS系统是用于全尺寸结构静力试验与分析的大型综合系统,目的之一就是为保证有限元分析和工程细节分析结果和试验测量结果的一致性和可靠性。对设计厂、所提供的强度校核的有限元模型如何修改后建立用于试验分析的有限元模型进行了论述。     

冷环境中人体热调节的数学模拟与研究

针对冷环境对人体的影响特点, 建立了冷环境中准三维人体热调节系统数学模型, 采用数值方法对人体热调节系统数学模型进行求解, 计算了不同冷环境条件下人体温度分布及动态响应, 计算结果与实验结果相符。     

随机取向短纤维增强SMC复合材料疲劳损伤模型

 讨论了复合材料疲劳损伤的数学描述方法，引用等效模量随疲劳过程的降低作为损伤的度量，借助于连续介质损伤力学ＣＤＭ，建立起损伤速率与循环次数之间的幂函数关系。试验发现，疲劳损伤的演变可分为３个阶段，而在一定的应力水平下，稳定扩展的第２阶段占据主导地位，为从理论上预测疲劳寿命成为可能。     

可压缩粘性流绕翼型的N─S方程自适应网格解

从Ｎ－Ｓ方程出发,采用ＬＵ－ＡＤＩ隐式分解方法求解绕翼型的可压缩粘性流动。湍流模式采用Ｂａｌｄｗｉｎ－Ｌｏｍａｘ代数湍流模式和ｑ－ω二方程微分模式以研究湍流边界层的非平衡效应;为更好地捕捉激波,对网格进行了自适应调整。通过对ＮＡＣＡ００１２和ＲＡＥ２８２２两种翼型在亚音速和跨音速不同马赫数和雷诺数下进行大量计算,表明该方法对改进湍流计算、提高激波分辨率有较好的效果     

结构有限元模型的试验建模

 对于复杂结构系统,用试验测取的模态参数来识别或修改系统的物理参数,以构造其动态数学模型。这种方法是建立振动系统数学模型的逆方法。 近些年来,国内外不少学者在这一领域做了很多工作。他们方法的共同点是识别系统的总质量矩阵和总刚度矩阵,因此未知量较多。考虑到结构系统总矩阵元素之间有一定关系,文献[3]讨论了一种建立动态有限元模型的逆方法。