SUBJECT INDEX OF CHINESE JOURNAL OF AERONAUTICS (2008)

Fluid Mechanics, Flight Mechanics and Engine Aerodynamic Design and Analysis of a Low-reaction Axial Compressor Stage (P) …………………… ………………………………… Qiang Xiaoqing, Wang Songtao, Feng Guotai, Wang Zhongqi (1) Active Aerothermoelastic Cont     

SUBJECT INDEX OF CHINESE JOURNAL OF AERONAUTICS （2007）

Fluid Mechanics, Flight Mechanics and Engine Integrated Entry Guidance for Reusable Launch Vehicle (P) ……………………………………………… ………………………………………………… Ning Guodong, Zhang Shuguang, Fang Zhenping (1) Experimental Investigation o     

SUBJECT INDEX OF CHINESE JOURNAL OF AERONAUTICS(2003)

(Started in1 965 ,a two-monthly in Chinese version)AerodynamicsHierarchical Evolutionary Algorithms and Its Application in Transonic Airfoil Optimization in Aerodynamics(P)…………WANG Jiang-feng,WU Yi-zhao(1 )………………………………………………………………………………………Single-Phase Forced Convection Heat Transfer in Micro Rectangular Channels(P) ZHAO Zeng-hui,YU Jian-zu(7)……Study on Breakup of Conical Liquid Sheetunder Varying Flow Conditions(TN)………………………………     

SUBJECT INDEX OF CHINESE JOURNAL OF AERONAUTICS（2004）

FluidMechanics ,FlightMechanicsandEngineResearchonEffectofOilFilmInertiaonPistonSkirtbyIterationMethod(P) ………………………………………………　　MENGFan ming ,ZHANGYou yun(1)…………………………………………………………………………………TheOptimizationMethodoftheSectorPartitionBasedonMetamorphicVoronoiPolygon(P)　　HANSong chen ,ZHANGMing(7)………………………………………………………………………………………StudyonFormsofVortexBreakdownoverDeltaWing(TN) LUZhi yong ,ZHULi g…     

SUBJECT INDEX OF CHINESE JOURNAL OF AERONAUTICS(2002)

AerodynamicsFinite Element Method forthe Transient Processof the Separation of External Storesfrom Aircraft ……………………YANG Zuo-sheng(1 )………………………………………………………………………………………………………Effectof Diffusively Shaped Holes on the Turbulent Flow Field of a Film Cooling Plate…………………………………SHIHong-hui,Kenji Kiriyama,Motoyuki Itoh(6)………………………………………………………………………Prediction of Aerodynamic Interactions of Helicopter Rot…     

Abstracts of Acta Aeronautica et Astronautica Sinica

(Started in 196 5 ,a two- monthly in Chinese version)ABSTRACTSDirect Prediction of the Effects of Mistuning on Vibrationof Bladed Disk Assemblies.ZHOU Chuan- yue,ZOU Jing-xiang(Dept.of Astronautics and Mechanics,Harbin Insti-tute of Technology,Harbin　 15 0 0 0 1,China) .Acta Aero-nautica et Astronautica Sinica (ISSN 10 0 0 - 6 893) ,Vol. 2 2 ,no.5 ,September 2 0 0 1,P4 6 5 - 4 6 7. 9refs.in Chinese.The rotational periodicity of bladed disk assem blies canbe destroyed by m an…     

Tensile properties analysis of CFRP-titanium plate multi-bolt hybrid joints

Hybrid joints have better tensile properties than pure bonded and bolted bolts, and are increasingly used in the aerospace field. Tensile tests are carried out for the Hybrid Bonded/Bolted(HBB) joints of Carbon Fiber Reinforced Polymer(CFRP) laminate and titanium alloy plate under different bolt numbers, and the corresponding load–displacement curves are obtained. At the same time, based on Continuum Damage Mechanics(CDM) theory, which is derived from 3D Hashin failure criteria, and a Cohesive Z...     

《飞行器测控技术》1997年总目录

测控总体 大气水平不均匀性对电波折射误差修正精度的影响………………………(一)P21—24 测量船船体辐射增温试验结果的初步分析………··………………………·(二)P10—14 欧空局的多任务地面基础设施(1996—2005)………………………………(二)P48—55 NASA任务操作与控制结构项目…………………………¨。………………(二)P56—61 对下一代卫星操作控制的系统研究…………………………………………(二)P62—67 天地分布智能化大系统分析…………………………………………………(三)P23—30 新世纪技术验证计划的小卫星通信……………     

JOURNAL OF AEROSPACE POWER(Quarterly) Subject Index Volume16 2 0 0 1

SPECIAL COLUMN:Development of China′s Aeroengines in2 1st CenturyDeliberation Upon Advance of Aeroengine Developmentin China LIU Da-xiang ( 7 )………………Performance-Related Key Technologies and Difficulties of Engines with Thrust to Weight Ratio upto Level of 15 CHEN Da-guang,etal ( 7 )…………………………………………………………Prospects of the Aeroengine Control Developmentin the Early Time of the2 1st CenturySUN Jian-guo( 10 2 )……………………………………………………     

Abstracts of Acta Aeronautica et Astronautica Sinica

(Started in 196 5 ,a two- monthly in Chinese version)ABSTRACTSDirect Prediction of the Effects of Mistuning on Vibrationof Bladed Disk Assemblies.ZHOU Chuan- yue,ZOU Jing-xiang(Dept.of Astronautics and Mechanics,Harbin Insti-tute of Technology,Harbin　 15 0 0 0 1,China) .Acta Aero-nautica et Astronautica Sinica (ISSN 10 0 0 - 6 893) ,Vol. 2 2 ,no.5 ,September 2 0 0 1,P4 6 5 - 4 6 7. 9refs.in Chinese.The rotational periodicity of bladed disk assem blies canbe destroyed by m anufacturing process,m aterial,a co...     

《飞行器测控技术》1994年总目录

测控总体 可靠性鉴定中利用验前信息的序贯验后加权方法…………………………“(一-)p.1—8 落点散布鉴定的最优统计决策………………………………………………”(--)p.1—7 确定星一一星跟踪区间的一种计算方法……………………………………(二)P.20—25 高级中继卫星系统计划概述…………………………………………………一(二)P.58二67 'I"DRSS利用成批最小二乘法和序贯法测定陆地星一4轨道精度评定……(--)p.68—80 欧洲数据中继系统的中继卫星………………………………………………(三)P.67—78 美国空军卫星控制网和国防部其它地面…     

JOURNAL OF CIVIL AVIATION INSTITUTE OF CHINA VOL.14 1996 CONTENS

NO.1（S——NO.43）FueMeterillgUnit·’………………·’…··’……’…………··’……“”…’“…………XuChunsheng（l）TheARllqC629DintalDataBusSpstem·’”””““·””’“”“””·“”“””·“””””““”””””””’”””’“““””“”DuMing（7ATeChrucalApproachotheEstablislll]:lelltofheWAASfortheCivilAvationofCina…’…·’…·’·‘·’……·’…··’…·’·励onQ沂uanat.al（lheOptionFamphina’sO讪AvationforitheApproachandLa讪旭SystemS“’“””·““”·“““…     

《航空动力学报》2006年(第21卷)分类索引

气动热力学与总体设计高精度数值方法在DNS中的应用……………………………………肖凯涛,刘吉平,朵英贤,等(1Ⅰ)使用GAO-YONG模型对不可压圆管湍流的计算…………………………………王绪伦,高歌(7Ⅰ)基于多目标遗传算法的航空发动机总体性能优化设计…………………李立君,尹泽勇,乔渭阳(13Ⅰ)涵道尾桨的CFD模拟与验证………………………………………………………于子文,曹义华(19Ⅰ)定常吹/吸气控制凸包分离的数值研究(简报)…………………季路成,林峰,Marco P Schoen(25Ⅰ)双模态冲压发动机进气道/隔离段流场的数值研究(简报)…………     

ACTA AERONAUTICA ET ASTRONAUTICA SINICA Series A (1989) Subject Index

F 1 uid MeehaniesConcePtual Study Methodologies for Advaneed AerosPaee Vehieles ...............................................................……Huang Zhicheng(Al)A New一yPe ofGas LubricatedFoilThrustBearing ........ ..............……,..................……Ke Wanzhen and Dong Weihua(Al0)Numerical Caleulations of HyPersonie Nonequilibrium Flow over a Blunt Wedge .................................……ShenJianweiandQuZhanghua(A67)A ComPutational Method ofAerodynamics for Subsoni…     

Closed form algorithm of double-satellite TDOA+AOA localization based on WGS-84 model

In this paper, we consider the double-satellite localization under the earth ellipsoid model of the Wideband Geodetic System(WGS-84) using the Time Difference of Arrival(TDOA)and the Angle-of-Arrival(AOA).Several closed-form solution algorithms via the pseudolinearization of the measurement equations are presented to efficiently estimate the location.These algorithms include the Weighted Least Squares(WLS), the Constrained Total Least Squares(CTLS), and the Taylor-Series Iteration(TSI).Performance comparison of the proposed methods with the Cramér-Rao Lower Bound(CRLB) in the simulation is shown to demonstrate that the proposed algorithms are feasible and have stable performance.     

ACTA AERONAUTICA ET ASTRONAUTICA SINICASeries B (1989) Subject Index

F luid MeehanieSI沈veloPment of a Seeond〔记neration Injeetor Driven Transonie Wind Tunnel at BUAA .........................……Ling YunPei,Zhang Hua and Liu Jian(Bg)Analysis of Leakage厂haracteristies of Labyrinth Seals··……Zhu Yizheng and He Feng(B15)on the Aeeelerating Airflow Problem in the Test Seetion of a Transonie Wind Tunnel·....·.····.........……,·.一.·................……乙eng Guofeng(B73)Aerodynamie Analysis and Modifieation氏sign of NPU Airfoils .. ..…     

PREFACE

High Performance Propulsion System Advanced Research Program(HPPSARP) is state-supported and carried out under the charge of Gas Turbine Establishment. HPPSARP has been making great contributions to catching up the advanced world levels and shortening technological gaps between PRC and developed countries. This special issue crystalizes the cream of HPPSARP's strength projects, which have come to the end. The other projects of the HPPSARP will be summed up into the coming special issues while completed.     

2005年《宇航材料工艺》总目次

□综述碳纳米管增强复合材料研究进展…………………………………………………………刘政赵素(1)耐超高温材料研究……………………………………………………刘军熊翔王建营黄伯云(1)MoSi2及其复合材料的研究进展…………………………………李玲艳艾云龙程玉桂刘长虹(1)非连续增强金属基复合材料的热残余应力………………………………………………胡明费维栋(1)介质材料复介电常数变温测量技术综述……………………………何小瓦李恩张其劭郭高凤(1)我国高性能烧蚀防热材料用酚醛树脂研究进展………………………………张衍刘育建王井岗(2)P…     

DIGITAL GENERATION OF TWO-DIMENSIONAL FIELD OF TURBULENCE FOR FLIGHT SIMULATION

In some special cases of flight simulation (e.g. for formation flight, in-flight tanking) it is required to generate a two-dimensional field of turbulence, in which the turbulent wind speeds are stochastic functions of two coordinates (e.g. x in the flight direction and y in the wing span direction). For this purpose a simple and efficient technique for the digital generation of a two-dimensional field of turbulence,i.e. for the production of turbulent speed sequences on a rectangular network, is proposed in this paper. The correlation of the turbulent field so generated is found to be in good agreement with the theoretical correlation of the turbulence model, and thus the feasibility of the proposed method is verified. Two possible operation modes (off-line and on-line) of the turbulence generator in flight simulation are also discussed.