为航天任务服务的地-地通信

本文叙述了目前的NASA通信同(NASCOM)以及该网为所有NASA航天计划提供长途工作通信的发展过程。还介绍了为满足80年代NASA远程通信要求而正在实施的一些方案和技术。     

高、低能扰动力函数对叶轮机阵发非定常气动力的影响(英文)

为了研究扰动力函数对多级叶轮机叶片排中基本的高、低能阵发非定常气动响应的影响,在研究用轴流压气机上进行了一系列的基础研究。      

TRANSIENT AERODYNAMIC BEHAVIOURS ASSOCIATED WITH STEPWISE INCIDENCE VARIATION OF AIRFOILS

Transient aerodynamic characteristics of airfoil are important for the safety of airplanes, the development of helicopter rotors and many other applications of unsteady aerodynamics. For a better understanding of these phenomena, it is necessary to investigate the simultaneous relation between the characteristics and the flow field. The purpose of the present study is to clarify experimentally the fundamentals of the aerodynamic behaviours associated with stepwise incidence variations from 0 to some certain values, including high angles of attack, of symmetric airfoils at low speeds, Reynolds number being of the order of 104. Temporal variations of surface pressure distribution, lift, drag and . pitching moment, and the observation of the flow field will be discussed.     

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,     

前掠翼根部流动分离的控制

 在风洞和水洞中研究了机翼根部修形、活动边条、固定边条、边条襟翼和链接边条在控制前掠翼根部流动分离方面的作用。分析了上述措施对机翼流动的干扰机理及其对气动性能的影响。研究结果表明,各种措施对控制前掠翼根部流动分离均有明显效果,可提高大迎角升阻特性,改善纵向力矩特性和配平能力。固定边条和边条襟翼还可改善中小迎角的升阻性能,链接边条和边条襟翼则可使失速性能提高。加鸭翼后上述气动收益更加明显。     

有关近赤道卫星圆轨道初始节点位置的一些有价值的分析结果

本文利用基于李氏变换的摄动理论,求得了近赤道卫星圆轨道倾角和升交点赤径的二阶长周期解。这种解包含了地球扁率与月—日摄动的平均效应。然后给出了对任务分析有用的三种算法。第一种算法求得了导致倾角减小至零的初始节点位置,以及达到零倾角所对应的时间;第二种算法确定了在给定的时间间隔内,使轨道倾角保持在规定值范围内的初始节点所在区域;第三种算法确定了在不采用任何机动控制的情况下,使卫星保持在规定倾角容差之内的时间最长的初始节点位置,并求出与之对应的最长时间。对于24小时近赤道卫星圆轨道,本文给出了第一和第三种算法的结果,并以简单的闭合形式给出。