Euler computation of the nearfield wake vortex of an aircraft in take-off configuration

Numerical simulations based on the three-dimensional Euler equations are used to investigate the predictive capability of an Euler code for calculations of the nearfield wake of a narrow-body airliner wind tunnel model in take-off configuration up to a half span behind the wing tip trailing edge. Simulation results on both structured and unstructured grids are presented. The results on the block-structured grid were obtained within the scope of the EU-project EUROWAKE. The simulation quality of the vortex formation and spatial development is analysed by comparison to wind tunnel measurements of the spanwise lift distribution available from the EU-project DUPRIN II and to experimental PIV data available from the EU-project EUROWAKE.     

The Main Results and the Perspectives in the Researches at SSRT

In this report briefly presented the contemporary state of the experimental base of Radio Astrophysical Observatory (RAO) of the Institute of Solar-Terrestrial Physics (ISTP), the methodology of radioheliographic monitoring of the solar corona, the SSRT database, the RAO Web-pages, factors limiting the effective use of SSRT. Here are formulated the original results of the basic directions of the solar activity researches and the problems solutions on SSRT: (1) active regions at various development stages, morphology, modeling,signs of energy accumulation and flares buildup, forecast of powerful flares; (2) scenario, topology and the fine temporal picture of flares development, signs of primary energy release, radio emission mechanisms, scatter effects of radio emission in turbulent corona, energetic particles fluxes; (3) filaments; (4) CME with the localization of their initiation at the solar disk background, development scenario of filament activation + CME +flare; (5) coronal holes, and (6) bright coronal points.      

Laser Hardening of Metals

The first experiments on hardening metals by laserpeening induced residual compressive stress in the sur-face of metals for improving their resistance to cracking,stress corrosion and fatigue took place more than 30years ago. However, only today, with the development ofhigh-intensity pulse repetitive rate lasers, this methodstarts to compete to traditional peening, which use influ-ence of small metal balls.Laser peening uses pulses with high intensity 109￣1010 W/cm2 [1]. The laser energy abso…     

Orbital corrections by a single-input impulsive control applied along the geomagnetic field

This paper examines the possibility of regular orbital corrections for a satellite controlled by an impulsive force applied along the induction vector of the local geomagnetic field. The main purpose of the correcting considered in the paper is to eliminate the drift in secular variation of the relative orbital parameters over the orbital period. The obtained results are applied to the formation flying problem. The developed method is tested using numerical simulation.     

KFTA太阳模拟器灯单元的方案设计

在进行KFTA太阳模拟器的设计中,首次采用了氙灯水平点燃的灯单元设计方案。氙灯水平点燃既可以提高太阳模拟器的能量利用率,又降低了成本,节省了人力、物力,但同样也面临着许多新的问题：灯的选择、灯的稳弧、灯的水平调节机构以及灯的应力分析等。文章正是从以上各个方面阐述了KFTA太阳模拟器灯单元的设计思想及方法。     

卫星动不平衡方法研究

文章结合在工程中遇到的动不平衡实际问题,根据平衡机的基本工作原理,提出了双平面分别配重、合成计算的解决思路,并在理论上对自旋稳定卫星的双平面配重的动不平衡配重的计算方法进行了分析和研究,验证了配平计算方法的正确性和可行性。最后,根据配重计算方法提出了配重调整的工艺步骤。     

碳/环氧复合材料层板基体裂纹的检测与分析

本工作从实验和计算两方面测算碳/环氧复合村料在拉伸载荷下,[0/90]s、[±45]_(s),]11=11]碳布三种层板基体裂纹发生的形式和应变水平,以期能预测不同裂纹产生的载荷门槛值。结果表明:采用声发射技术跟踪配合显微观测碳/环氧层板初始损伤(基体裂纹、脱层等)的应力水平,并采用能量判据有限无计算裂纹扩展的临界应变能释放率,计算和实验结果比较,符合较好。     

Understanding solar streamers: The role of SOHO

Streamers have been observed since far back in time, but our knowledge of their morphology and of their physical characteristics is still very limited. As a consequence, the present streamer picture is largely incomplete: because individual features are poorly known, their role in more general phenomena (like the evolution of the global corona or the solar wind mass and flow pattern) is also poorly known. In this presentation, the more relevant open problems in the understanding of streamers will be illustrated and it will be shown how new data acquired by SOHO may help us to reach a better understanding of these structures.     

XMM-Newton observations across the Cygnus Loop from northeastern rim to southwestern rim

We have observed the Cygnus Loop from the northeast (NE) to the southwest (SW) with XMM-Newton. We extracted spectra from 3′-spaced annular regions across the Loop and fitted them either with a one-kT_e-component non-equilibrium ionization (NEI) model or with two-kT_e-component NEI model. We found that the two-kT_e-component model yields significantly better fits in almost all the spectra than the one-kT_e-component model. Judging from the abundances, the high-kT_e-component in the two-temperature model must be fossil ejecta while the low-kT_e-component comes from the swept-up interstellar medium (ISM). The distributions of Ne, Mg, Si, and S for fossil ejecta appear to retain the onion-skin structure at the time of a supernova explosion, suggesting that significant overturning of the ejecta has not occurred yet. Comparing the relative abundances of fossil ejecta estimated for the entire Cygnus Loop with those from theoretical calculations for Type-II SN, the mass of the progenitor star is likely to be ∼13 M_⊙. The trends of the radial profiles of kT_e and emission integral for the swept-up ISM are adequately described by the Sedov model, suggesting that the swept-up ISM is concentrated in a shell-like structure. Comparing our data with the Sedov model, we found the ambient medium density to be ∼0.7 cm⁻³. Then, we estimated the total mass of the swept-up ISM and the age of the remnant to be ∼130 M_⊙ and 13,000 years, respectively. Note that if the explosion occurred within a stellar wind cavity, then the density in the cavity, the total swept-up mass in the cavity, and the age of the remnant are estimated to be ∼0.14 cm⁻³, ∼25 M_⊙, and ∼10,000 years, respectively.     

应用试验模态参数修正理论模型的最佳矩阵逼近法

本文从特征方程和模态正交性条件出发，给出了一种应用模态参数识别结果修正理论模型的最佳矩阵逼近方法。该方法通过对识别出的模态矩阵进行奇异值分解并结合特征方程和模态正交条件导出了修正理论模型的通解表达式，在此基础上，给出了最佳逼近解的定义，研究了最佳逼近解的唯一性，给出了最佳修正质量矩阵和刚度矩阵的具体表达式，数值计算表明，本文方法具有很高的修正精度，对于大误差模型也有较好的修正能力，具有一定的应有和