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Acta Aeronautica Et Astronautica Sinica
FQ: 月刊
AD of Publication: 北京市
Lanuage: 中文;
ISSN: 1000-6893
CN: 11-1929/V
YP: 1965
Url: 中国航空学会;北京航空航天大学
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Acta Aeronautica Et Astronautica Sinica
2002 -02
Catalog
DAMAGE MECHANICS—ADDITIONAL LOAD—FINITE ELEMENT METHOD FOR FATIGUE LIFE PREDICTION OF AXISYMMETRICAL STRUCTURAL MEMBERS TANG Xue song\+\{1,2\}, YANG Ji yun\+1, JIANG Chi ping\+1, ZHANG Xing\+1 (1.Department of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronatics and Astronatics, Beijing\ 100083, China) (2. Department of Bridge and Structure E
THERMAL PROPERTY OF 3-D BRAIDED FIBER COMPOSITES: EXPERIMENTAL AND NUMERICAL RESULTS CHENG Wei 1, ZHAO Shou gen 1, LIU Zhen guo 1, FENG Zhi hai 2, YAO Cheng zhao 2, YU Rui lian 2 (1. Solid Mechanics Research Center, Beijing University of Aeronautics & Astronautics, Beijing\ 100083, China) (2. Aerospace Research Institute of
3D FINITE ELEMENT ANALYSIS OF SIF OF THE STRUCTURE WITH DIMPLE HOLE SHEN Hai\|jun, GUO Wan\|lin (Aerocraft Department, Nanjing University of Aeronautics & Astronautics, Nanjing\ 210016, China)
MODEL OF RELIABILITY GROWTH EVALUATING TO VARIOUS ENVIRONMENTS ZHAO Yu, HUANG Ming, WANG Zhi (Institute of Reliability Engineering, Beijing University of Aeronautics and Astronatics, Beijing 100083, China)
DESIGN OF GUIDANCE AND CONTROL SYSTEM FOR HIGH SPEED REENTRY AEROCRAFT LIAN Bao hua, CUI Ping yuan, CUI Hu tao (Deep Space Exploration Research Center, Harbin Institute of Technology, Harbin 150001, China)
AIRBORNE FDDI HIGH-SPEED DATA COMMUNICATION SYSTEM WANG Shi kui 1, TIE Man xia 2, YANG Jian xi 1 (1. Chinese Aeronautic Computing Technique Research Institute, Xi′an\ 710068, China) (2. Information Science Institute, Xidian University, Xi′an\ 710071, China)
APPLICATION OF GENERALIZED SINGULAR PERTURBATION APPROXIMATION METHOD TO CONTROLLER REDUCTION ZHANG Li jun 1, ZENG Jian ping 2, CHENG Peng 2 (1. Computer Science & Engineering Department, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) (2. Automatic Control Department, Beijing University of Aeronautics and Ast
NEW POLE ASSIGNMENT APPROACH FOR GENERALIZED PREDICTIVE CONTROL SHI Wu\|xi, HUO Wei, BI Shu\|sheng, ZONG Guang\|hua (The Seventh Research Division, Beijing University of Aeronautics Astronautics, Beijing\ 100083, China)
GENERALIZED HELICAL MOVEMENT AND GEOMETRIC MODELING OF COMPLICATED-SHAPE REVOLVING CUTTING TOOLS HE Yao\|xiong, ZHOU Yun\|fei, ZHOU Ji (National ERC of CNC System, Huazhong University of Science & Technology, Wuhan\ 430074, China)
INFRARED EMISSIONS FROM TURBOJET WITH TWO-DIMENSIONAL NOZZLE ZHENG Li\|bao (Nanjing University of Aeronautics and Astronautics, Nanjing\ 210016, China)
RESEARCH AND APPLICATION OF VISCOELASTIC MATERIAL ON MODELING OF SANDWICH PLATE WITH VISCOELASTIC CORE LIU Tian xiong 1, HUA Hong xing 2, CHEN Zhao neng 1 (1. School of Mechanical Engineering, Shanghai Jiaotong University, Shanghai\ 200030, China) (2. State Key Laboratory of Vibration, Shock and Noise, Shanghai Jiaotong University, Shanghai\ 2000
STUDY OF DOUBLE-LAYER CERAMIC COMPLEX ARMOR FOR DEFENSIBLE PERFORMANCE DU Zhong\|hua, ZHAO Guo\|zhi, WANG Xiao\|ming, SHEN Pei\|hui (School of Mechanics, Nanjing University of Science & Technology, Nanjing\ 210094, China)
INVESTIGATION INTO THE TENSILE CONSTITUTIVE RELATION AND FAILURE MECHANISM OF PUR FOAMED PLASTICS LU Zi xing 1,2 (1. Institute of Solid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China) (2. Laboratory for Nonlinear Mechanics of Continuous Media, Institute of Mechanics, Chinese Academy of Sciences, Beijing
PROBABILISTIC NEURAL NETWORKS BASED ENGINE FAULT DIAGNOSIS YE Zhi\|feng, SUN Jian\|guo (College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing\ 210016, China)
GENERAL IMPACT ANALYSIS MODEL AND LOW-VELOCITY IMPACT RESPONSE ALGORITHM DUAN Shi hui 1, YE Tian qi 2 (1. Aircraft Strength Research Institute of China, Xi′an 710065, China) (2. Department of Aircraft, Northwestern Polytechnical University, Xi′an 710072, China)
EVALUATION OF VICSO-PLASTICITY OF POWDER METALLURGY SUPERALLOY BY EXPERIMENT AND ESTIMATION OF CONSTITUTIVE PARAMETERS SONG Ying dong, GAO De ping, YANG Zhi guo (1. Institute of Energy and Power, Nanjing University of Aeronautics and Astronautics, Najing 210016, China) (2. 608 Research Institute, Zhuzhou 412002, China)
STUDY OF COMPRESSIBLE NONPARALLEL FLOW STABILITY FOR BOUNDARY LAYERS TANG Deng\|bin, MA Qian\|rong, CHEN Guo\|wei [WT5”BZ](Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Nanjing\ 210016, China) [WT5”HZ]
IMPROVEMENT STUDY ON AERODYNAMIC CHARACTERISTICS OF A FIGHTER CONFIGURATION WITH STRAKE-WING LU Zhi yong, GAO Wei ming (Institute of Fluid Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China)
STUDY ON NUMERICAL METHOD FOR DETERMINING THE DROPLET TRAJECTORIES YANG Qian, CHANG Shi nan, YUAN Xiu gan (Faculty 505, Beijing University of Aeronautics and Astronautics, Beijing\ 100083, China)
MULTI-OBJECTIVE AIRFOIL OPTIMIZATION USING PARETO GENETIC ALGORITHM SUI Hong tao, CHEN Hong quan, HUANG Ming ke (Faculty 601, Nanjing University of Aeronautics and Astronautics, Nanjing\ 210016, China)
OPTIMIZATION AND PERFORMANCE ANALYSIS OF DISTRIBUTED OS-CFAR DETECTION BASED ON NICHE GENETIC ALGORITHMS WANG Ming yu 1, YU Bian zhang 2 (1. Missle Institute, AFEU, Sanyuan\ 713800, China) (2. Department of Electrical Engineering, Northwestern Polytechnical University, Xi′an\ 710072, China)
SATELLITE FAULT DIAGNOSIS BASED ON OPTIMAL PARITY VECTOR METHOD YANG Jing, ZHANG Hong yue (Faculty 301, Beijing University of Aeronautics and Astronautics, Beijing\ 100083, China)
SPECTRAL DENSITY OF π-TIME-FREQUENCY-SHIFT-KEYING SIGNAL ZHOU Li, WANG Qi, GU Ping (Nanchang Institute of Aeronautical Technology, Nanchang\ 330034, China)
NEW CONSTITUTIVE EQUATION BASED ON PARALLEL MODEL FOR Ti-6Al-4V ALLOY NIE Lei, LI Fu guo, FANG Yong (College of Mater. Sci. and Engin., Northwestern Polytechnical University, Xi′an\ 710072, China)
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