1672-6553
2014 Issue 3
PROGRESS IN SPACECRAFT VIBRATION TESTING CONTROL TECHNOLOGY
Ci Yongwei;,Fu Leping;,Shao Xiaoping;, Qiu Dalu;
Ci Yongwei;,Fu Leping;,Shao Xiaoping;, Qiu Dalu;
..............page:193-200
FLUTTER ANALYSIS OF 2-D AIRCRAFT WINGS IN SUPERSONIC FLOW
Chen Yushu;,Ye Xin;
Chen Yushu;,Ye Xin;
..............page:201-204
SPACE STRUCTURE VIBRATION CONTROL BASED ON PASSIVE NONLINEAR ENERGY SINK
Chen Liqun;,Ding Hu;,Yang Kai;,Zang Jian;,Zhang Yewei;
Chen Liqun;,Ding Hu;,Yang Kai;,Zang Jian;,Zhang Yewei;
..............page:205-209
DYNAMCIS AND CONTROL OF AN OSCILLATOR WITH VISCOELASTIC ITEM
Luo Jiawei;,Xu Xu;
Luo Jiawei;,Xu Xu;
..............page:210-214
STUDY ON ACTIVE CONTROL FOR PARAMETRIC VIBRATION SYSTEM
Fu Chenchen;,Huang Dishan;
Fu Chenchen;,Huang Dishan;
..............page:215-219
DYNAMIC SIMULATION ABOUT THE PARALLEL MULTI CONNECTING ROD SAMPLE CAPTURING MECHANIC
Li Dongying;,Liu Hanwu;,Zhang Hua;
Li Dongying;,Liu Hanwu;,Zhang Hua;
..............page:220-224
SIMULATION OF 'TAIL-SLAP'PHENOMENON OF SUPERCAVITATING PROJECTILES WITH FLUID/STRUCTURE INTERACTION
He Qiankun;,Wang Cong;,Wei Yingjie;
He Qiankun;,Wang Cong;,Wei Yingjie;
..............page:225-229
ON-ORBIT LOAD COMPUTATION AND ANALYSIS OF FLEXIBLE SOLAR ARRAY FOR CHINA SPACE STATION
Guo Qiwei;,Liu Fang;,Wu Song;,Xiao Yuzhi;
Guo Qiwei;,Liu Fang;,Wu Song;,Xiao Yuzhi;
..............page:230-234
THE ANALYSIS OF VIBRATION REDUCTION CHARACTERISTICS OF PAYLOAD SUPPORTED BAY
Hu Dike;,Liu Zhengyong;,Qin Chuan;,Shen Lin;
Hu Dike;,Liu Zhengyong;,Qin Chuan;,Shen Lin;
..............page:235-238
THE ANALOGY METHOD TO COUPLING ANALYSIS OF ROCKETS CONSIDERING PROPELLANT SLOSHING
Tang Guoan;,Zhang Meiyan;,Zhu Changfan;
Tang Guoan;,Zhang Meiyan;,Zhu Changfan;
..............page:239-242
ANALYSIS IN THE WINDAGE OF ASD OUTSIDE THE FREQUENCY BANDWIDTH IN RANDOM VIBRATION TESTING
Ci Yongwei;,Fu Leping;,Qiu Dalu;,Shao Xiaoping;
Ci Yongwei;,Fu Leping;,Qiu Dalu;,Shao Xiaoping;
..............page:243-247
THE MEASURING METHOD OF KINEMATIC VECTOR PARAMETE
Li Wei;,MDGERAIMCHUK;,VPZINCHENKO;,Yuan Laohu;
Li Wei;,MDGERAIMCHUK;,VPZINCHENKO;,Yuan Laohu;
..............page:248-252
MULTI-OBJECTIVE TOPOLOGY OPTIMIZATION DESIGN METHOD BASED ON PENALIZED DENSITY THEORY FOR AIRCRAFT LIFTING-SURFACE
Liu Guang;,Miao Xiaoting;,Xu Quan;,Zhang Fenggang;
Liu Guang;,Miao Xiaoting;,Xu Quan;,Zhang Fenggang;
..............page:253-258
A HYBRID METHOD FOR THE ANALYSIS OF STRUCTURAL VIBRATION IN MEDIUM FREQUENCY
Wang Kun;,Zhang Bin;,Zhao Yang;
Wang Kun;,Zhang Bin;,Zhao Yang;
..............page:259-263
EFFECT ANALYSIS OF SPACE DOCKING MECHANISM BUFFERING TEST TABLE UPON THE CONNECTION AND SEPARATION EXPERIMENT
Xiao Yuzhi;,Zhang Hua;
Xiao Yuzhi;,Zhang Hua;
..............page:264-268
AN AUTOMATIC IDENTIFICATION METHOD FOR LONGITUDINAL MODES OF STRUCTURAL SYSTEM OF ROCKET
Fang Bo;,Tang Ye;,Yang Feihu;,Zang Jian;,Zhang Yewei;
Fang Bo;,Tang Ye;,Yang Feihu;,Zang Jian;,Zhang Yewei;
..............page:269-273
RESEARCH ON ENGINEERING PRACTICE OF MODAL ANALYSIS-TEST OF SPACECRAFT
Guo Qiwei;,Liu Fang;,Wu Song;,Zhao Yangdong;
Guo Qiwei;,Liu Fang;,Wu Song;,Zhao Yangdong;
..............page:274-278
THE METHOD OF TIME WAVEFORM REPLICATION TRANSIENT VIBRATION TEST BASED ON ENERGY SPECTRUM DENSITY
Liu Hefeng;,Wang He;,Yang Feihu;
Liu Hefeng;,Wang He;,Yang Feihu;
..............page:279-282
A NEW METHOD ON FLUTTER TAILORING TECHNIQUES OF HIGH-ASPECT-RATIO WINGS
Ding Yuliang;,Jin Haibo;,Ren Zhiyi;
Ding Yuliang;,Jin Haibo;,Ren Zhiyi;
..............page:283-288