弧齿锥齿轮的齿距误差对传动性能的影响研究

采用齿轮啮合仿真和承载啮合仿真技术 ,对重合度达到 2 .0的航空弧齿锥齿轮的齿距误差的影响进行了研究。首先定义了航空弧齿锥齿轮相对齿距误差 ,选取了量级 ,研究了这一误差对齿轮实际重合度、传动误差、齿面载荷分布和齿间载荷分配的影响。进一步又分析了在一定齿距误差下载荷变化的影响以及固定载荷下误差变化的影响 ,为高重合度航空弧齿锥齿轮的应用提供了依据     

多块网格网络并行计算中的负载分配研究

针对CFD中多块网格计算的特点，并使用MPI网络并行系统，对某战斗机绕流进行了基于三维Euler方程的并行计算，主要研究了多块网格并行计算中负载的分配方法，发展了负载自动分配和网格自动重分区程序，计算结果表明：并行计算结果和实验结果完全吻合，8个节点机的并行效率达到了89％。     

Analysis of some modified ordered statistic CFAR: OSGO and OSSOCFAR

It is necessary for automatic detection radars to be adaptive to variations in background clutter in order to maintain a constant false alarm rate (CFAR). A CFAR based on an ordered statistic technique (OS CFAR) has some advantages over the cell-averaging technique (CA CFAR), especially in clutter edges or multiple target environments; unfortunately the large processing time required by this technique limits its use. The authors present two new OS CFARs that require only ahlf the processing time. One is an ordered statistic greatest of CFAR (OSGO), while the other is an ordered statistic smallest of CFAR (OSSO). The OSGO CFAR has the advantages of the OS CFAR with only a negligible increment to the CFAR loss     

基于共轭方程法的跨音速机翼气动力优化设计

 设计状态的机翼气动力特性是设计人员最为关心的指标, 应用控制理论设计方法进行了有升力约束情形下跨音速机翼阻力优化设计研究, 根据给定的目标函数推导了相应的共轭方程和边界条件, 研究了共轭方程的数值求解方法, 以及计算目标函数对设计变量的敏感性导数时所涉及的度量矩阵变分求解问题, 研究了流场计算、共轭方程数值求解、敏感性导数求解和拟牛顿优化算法这几个主要方面的有效结合问题, 发展出了一种跨音速机翼气动力优化设计方法, 进行了跨音速机翼气动力优化设计研究验证, 优化后机翼气动力特性有一定程度的改善, 阻力系数能减少20%左右, 而升力系数有所增大, 说明所发展的设计方法是成功的, 该设计方法在跨音速及复杂外形气动设计方面比以往设计方法具有更好的适用性和优越性。     

亚声S型进气道模型吹风试验特性的研究

采用半经验的方法，对某S型进气道的模型试验数据进行了回归，建立了弹用涡喷（扇）发动机常用S型高亚声速进气道总压恢复系数与习行马赫数Ma，流量系数ψ，攻角α和侧滑角β的相关函数关系。该关经验公式可用于发动机稳态和启动加速过程一元数值仿真模型，从而提高一元发动机性能数值仿真计算的准确性。     

高重合度弧齿锥齿轮的强度分析

本文采用有限元应力影响矩阵法研究了高重合度弧齿锥齿轮在多种误差和载荷条件下的弯曲应力状态 ,证明了经过优化设计的高重合度弧齿锥齿轮不仅有良好的动态性能 ,而且在一定误差范围内在强度方面具有优越性     

XMM-Newton observations of low luminosity Be/X-ray candidates

A small number of early Be stars exhibit X-ray luminosities intermediate between those typical of early type stars and those radiated by Be/X-ray binaries in the quiescent state. We report on XMM-Newton observations of two such Be stars, HD 161103 and SAO 49725 which were originally discovered in a systematic cross-correlation between the ROSAT all-sky survey and SIMBAD. The new observations confirm the X-ray luminosity detected by ROSAT (L_X  10³² erg s⁻¹) and the hardness of their X-ray spectra (thin thermal with kT  8–10 keV or power law with photon index of 1.7) which are both unusual for normal early type stars. We discuss the possible origin of this excess X-ray emission in the light of the models proposed for γ-Cas, magnetic disc-star interaction or accretion onto a compact companion object, neutron star or white dwarf, and compare the properties of these two sources with those of the new massive systems discovered in the XMM- Newton/SSC survey of the Galactic plane.     

Structural development of the X-ray limb flare of 30 April 1980

We describe the development of the limb flare of 30 April 1980, 20:20 UT, as observed by the Hard X-ray Imaging Spectrometer (HXIS) aboard the Solar Maximum Mission (SMM). It consisted of a short-lived bright nucleus (FWHM < 10,000 km), just inside the Sun's limb; a longer lasting tongue, extending to a height of 30,000 km, and a more complicated feature, approximately situated at the Sun's limb. The tongue was a pre-existing magnetic structure that started emitting X-rays only a few seconds after the bright nucleus, and which had a slightly higher temperature than the nucleus; its X-ray emission may be caused by electrons escaped from the nucleus.     

REMS: The Environmental Sensor Suite for the Mars Science Laboratory Rover

The Rover Environmental Monitoring Station (REMS) will investigate environmental factors directly tied to current habitability at the Martian surface during the Mars Science Laboratory (MSL) mission. Three major habitability factors are addressed by REMS: the thermal environment, ultraviolet irradiation, and water cycling. The thermal environment is determined by a mixture of processes, chief amongst these being the meteorological. Accordingly, the REMS sensors have been designed to record air and ground temperatures, pressure, relative humidity, wind speed in the horizontal and vertical directions, as well as ultraviolet radiation in different bands. These sensors are distributed over the rover in four places: two booms located on the MSL Remote Sensing Mast, the ultraviolet sensor on the rover deck, and the pressure sensor inside the rover body. Typical daily REMS observations will collect 180 minutes of data from all sensors simultaneously (arranged in 5 minute hourly samples plus 60 additional minutes taken at times to be decided during the course of the mission). REMS will add significantly to the environmental record collected by prior missions through the range of simultaneous observations including water vapor; the ability to take measurements routinely through the night; the intended minimum of one Martian year of observations; and the first measurement of surface UV irradiation. In this paper, we describe the scientific potential of REMS measurements and describe in detail the sensors that constitute REMS and the calibration procedures.