SEPARATED FLOW AROUND BENT-NOSE BICONIC IN HYPERSONIC FLOW

This article investigates the separated flow around the bent-nose biconic, in which the second ordered TVD(Total Variation Diminishing) method is applied. The governing cqua-tion is a thin layer Navier-Stokes equation. The surface pressure distribution at the leeward side is a little higher in the vicinity of the symmetrical plane. This seems to be caused by the development of the vortex at the leeward side due to the separated flow. The location of a separation line and the size are in very good agreement with the experiment. Also the secondary separation is captured very clearly.     

OPTICAL TELEPHONE CORD PASSING THROUGH LONG PIPE WITH SPIRAL FLOW

A new effective technique, useful in telecommunications industry for passing an optical telephone cord attached to a connector through pipeline,has been developed using the spiral flow. Using this technique, the cord could be passed through a straight pipeline 150 meters long and a roll of vinyl tube 50 meters long. However, under the same condition, the cord could not pass through when using the turbulent flow. To obtain a high speed stable spiral flow, a nozzle with an annular slit connected to a conical cylinder was used. A pressurized fluid with no tangential flow was supplied through this slit and the fluid, passing through the conical cylinder, was deformed into spiral flow with the steeper axial velocity distribution compared to that of turbulence pipe flow due to Coanda effect and instability. As a result, the cord was attracted to the axis area of the pipe, which effectively increased the ability for the work of cord passing. This high ability for cord passing is attributed mainly to the reduct     

STRATOSPHERIC LIGHTER-THAN-AIR POWERED PLATFORM

A feasibility study has been carried out on a high altitude (20km) superpressurcd PLTA(powered lighter-than-air) platform, which has a long service life and larger payload than that of a large artificial satellite. This PLTA platform has an electric propulsion system to cope with wind flow for position keeping and its thruster is driven by solar power acquired through solar cells. Solar energy is to be stored for night use in regenerative fuel cells. The study is focused on energy balance and hull structure analysis of the platform. This platform is particularly capable of conducting high resolution remote sensing and telecommunications relay. This platform can replace a number of ground-based telecommunications relay facilities and can guarantee reasonable radio frequency intensity enough to secure good telecommunications quality. The altitude where the platform resides is the least windy area in the lower stratosphere at a height from which one can have a direct line of sight on the ground within a 1,     

摆动磨削和强力(蠕动进给)磨削方法的发展现状和应用可能性

为了使平面和型面磨削这种方法的应用更广泛、更有效和更经济早在五十年代的中期,Edmund Lang 就已集中了一些助手,从事于寻找进行平面和型面磨削新方法的可能性。即利用一种新型机床,它既能达到当时在铣床上所能达到的切削效率,同时也能达到一般磨削所能达到的精度。在当时现有的经验基础上作进一步发展,有可能在一定的前提和考虑到一些影响因素(磨轮、驱动功率、机器设计)的情况下实现这     

薄壁镁合金铸件砂型涂料的研究

随着现代航空与宇航技术的发展,大型薄壁铝、镁合金砂型铸件的应用日益增多。这类铸件的特点是尺寸大,壁厚小,结构复杂。在浇注过程中,往往在型腔未完全充满之前,金属液就失去了流动性,因而造成冷隔与欠铸。为此,解决成型质量问题就成为铸造大型薄壁铸件的一项重要课题。通常是采用提高合金浇注温度的办法,来满足薄壁铸件的成型需要。但是在某些情况下,这种办法并不能彻底解决薄壁铸件的     

飞行模拟的准直显示

本文叙述了目视飞行模拟器在显示方面的限制,表明了准直显示的要求。给出了获得飞行模拟准直显示法广泛研究的结果以及继之发展的“睹飞”(Duo-view)显示,从座舱各部分看,它都给出了不变形的显示。本文叙述了这种显示系统并指出了它的性能。     

光学薄膜的特性

本文研究介质薄膜的各种特性:折射率和吸收系数、光散射、结构、显微结构、密度、气体吸收、化学成分、均匀度、附着力、硬度和机械应力、环境影响。Ⅰ、前言适当地选择折射率、薄膜厚度和膜层数目,可以设计出各种通常是很复杂的光学薄膜,这种薄膜设计,要在工业上得以实现,是需要足够数量的高质量镀膜材料,经过处理之后,使薄膜有适当的复现特性。尽管在过去几年中材料科学和镀膜技术有显著的进展,但遗憾的是适合的材料数目仍然有限。单层薄膜的主要介质材料的基本光学性质的研究是 Hass     

计算流体动力学的问题范围及最新发展

1、引言本文是关于计算流体动力学问题范围和最新发展的译述。所谓“最新”是相对于我的书(Roache,1972)而言的。(为简短起见,那本书在本文中称为 CFD。本文里的有些课题在 CFD 中已提及但强调得不够,而其余的在写那本书时尚未出现。     

碳纤维增强塑料波纹结构圆椎壳体的研制

1.0 引言艾尔诺宇航技术公司用碳纤维增强塑料自行研制了转接器(俗称过渡段),已试制成功并经过了静力试验。这是一件波形结构形式的、有一个隔框加强的圆锥形外壳,此壳体的平均直径为900毫米,高度大约500毫米。这个筒式接头在卫星与运载火箭中间作     

用积分法解层流附面层分离问题的补充关系式的使用

在满足局部相似性的假设下,用附面层方程来导出积分量之间的关系。而得到的函数关系式可用作求解一般积分方程组的补充关系式。以具有热传导的平面屏前分离区问题作为例子,来说明这些补充关系的使用,用积分法来解这个问题。在冷表面上分离区的计算中,为了排除许多疑难问题,在分离点的上游使用了 Curle 通用压强曲线。计算结果与试