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GAS TURBINE ENGINE CONDITION MONITORING AND FAULT DIAGNOSTICS
Chen Daguang
1989, (6): 225-236.
PDF [ 789 K ]( 653 ) HTML
MODAL AGGREGATION AND ITS APPLICATION IN FLIGHT MECHANICS
Han Chao
1989, (6): 237-245.
PDF [ 455 K ]( 376 ) HTML
A FINITE ELEMENT ANALYSIS OF NONLINEAR INSTABILITY FOR LAMINATED COMPOSITE CYLINDRICAL SHELLS WITH LONGITUDINAL STIFFENERS AND TRANSVERSE FRAMES
He Jianguo;Hu Xunchuan;Li Songnian;Xing Tianan
1989, (6): 246-253.
PDF [ 431 K ]( 451 ) HTML
SEVERAL MODELS TO PREDICT THE LOW CYCLIC CORROSION FATIGUE LIFE
Jiang Zuguo
1989, (6): 254-258.
PDF [ 330 K ]( 368 ) HTML
A HYBRID-STRESS ELEMENT FOR BENDING ANALYSIS OF COMPOSITE LAMINATED PLATES
Duan Shihui;Jiang Bingguang
1989, (6): 259-263.
PDF [ 265 K ]( 347 ) HTML
PREDICTION OF TRANSMISSION LOSS THROUGH AN AIRCRAFT SIDEWALL USING STATISTICAL ENERGY ANALYSIS
Ming Ruisen;Sun Jincai
1989, (6): 264-271.
PDF [ 473 K ]( 339 ) HTML
DIGITAL CONTROL EXPERIMENT RESEARCH ON THE ENGINE JT15D-4
Ma Rei;Jiang Dazhong;Li Yuanye;Le Huacong
1989, (6): 272-279.
PDF [ 488 K ]( 373 ) HTML
THE EIGENVALUE SENSITIVITY ANALYSIS AND DESIGN FOR INTEGRATED FLIGHT/PROPULSION CONTROL SYSTEMS
Shen Gongzhang;Chen Zongji;Peng Kemao
1989, (6): 280-287.
PDF [ 431 K ]( 378 ) HTML
TEMPTATION TECHNIQUE OF TWO-POINT-SOURCE COUNTERACTING ARM
Si Xicai;Zha Yufeng
1989, (6): 288-296.
PDF [ 506 K ]( 438 ) HTML
SUB-OPTIMAL CONTROL FOR AIRBORNE TRACKING RADAR
Jin Dekun
1989, (6): 297-308.
PDF [ 618 K ]( 1230 ) HTML
APPLICATION INVESTIGATION ON SUPERPLASTIC FORMING /DIFFUSION BONDING COMBINED TECHNOLOGY OFTITANIUM ALLOY TC4
Wang Baoren;Ji Wenhai
1989, (6): 309-314.
PDF [ 563 K ]( 1419 ) HTML
THE EXPERIMENTAL INVESTIGATION ON THE SURFACE INTEGRITY CREATED BY CREEP FEED GRINDING OF DIFFICULT-TO-MACHINE MATERIALS
Wang Weilian;Jing Changsheng
1989, (6): 315-323.
PDF [ 516 K ]( 346 ) HTML
WALL INTERFERENCE CORRECTION OF HIGH-LIFT MULTI-COMPONENT AIRFOILS
Zhang Wenhua
1989, (6): 324-329.
PDF [ 342 K ]( 286 ) HTML
STRUCTURAL OPTIMIZATION WITH CONSTRAINT OF STRUCTURAL SYSTEM RELIABILITY
Pei Zhongxiu;Zhan Chengyu;Huang Wenmin;Zhang Shulin
1989, (6): 330-334.
PDF [ 272 K ]( 319 ) HTML
EXTENDED FINITE ELEMENT ANALYSIS FOR TWO DIMENSIONAL TEMPERATURE FIELD PROBLEMS
Gu Tianlog
1989, (6): 335-338.
PDF [ 259 K ]( 356 ) HTML
THE INVESTIGATION OF STRESS AT AN ENTER-GAS NOZZLE OF MAIN LANDING GEARS FOR FIGHTER AEROPLANES
Xie Yonghua;Zheng Sitao;Cui Zhenyuan
1989, (6): 339-341.
PDF [ 316 K ]( 348 ) HTML
NUMERICAL APPROACHES FOR SOLVING PARAMETRIC VIBRATION PROBLEMS IN HELICOPTER DYNAMICS
Yang Kaitian
1989, (6): 342-346.
PDF [ 277 K ]( 301 ) HTML
SUPERCONDUCTING GYROSCOPE
Li Shufang
1989, (6): 347-348.
PDF [ 120 K ]( 590 ) HTML
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