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20 May 2008, Volume 29 Issue 3

Avionics and Autocontrol

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20 May 2008, Volume 29 Issue 3

Fan/Compressor Aero Design Technology for High Bypass Ratio Turbofan
Abstract( 2756 )

Chen Maozhang;Liu Baojie

2008, (3): 513-526.

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Experimental Study of Airframe Noise with Improved Data Reduction Method of Microphone Array Measurements
Abstract( 2261 )

Qiao Weiyang;Ulf Michel

2008, (3): 527-533.

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Noise Radiation of Large-scale Commercial Aircraft in Take-off and Landing
Abstract( 2203 )

Qiao Weiyang;Xu Kaifu;Wu Zhaowei;Huang Wenchao;Qin Haoming

2008, (3): 534-541.

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Modeling and Experimental Study about the Heat Transfer in Micro Turbine Engine
Abstract( 2307 )

Huang Guoping;Liang Dewang;Ma Xiangdong;Zhang Qiang

2008, (3): 542-547.

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Fault Diagnosis Algorithm for Heat Exchanger of  Aircraft Environment Control System Based on Double Model Filter
Abstract( 2665 )

Pang Liping;Qu Hongquan;Dong Sujun

2008, (3): 548-553.

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Integrated Design Optimization of Turbofan Engines Cycle for Multi-role Fighters
Abstract( 2816 )

Chen Yuchun;Wang Xiaofeng;Tu Qiuye;Zhang Hong;Cai Yuanhu

2008, (3): 554-561.

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Discussion of Design Methods for Silent and Fuel Efficient Medium Range Civil Transport
Abstract( 2624 )

Zhu Ziqiang;Wang Xiaolu;Wu Zongcheng;Chen Zemin

2008, (3): 562-572.

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Structure Technology Development of Large Commercial Aircraft
Abstract( 2374 )

Cui Degang

2008, (3): 573-582.

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The Study of Concept Design Criteria for Large-scale Passenger Aircraft with New Technologies
Abstract( 2800 )

Song Bifeng;Zhang Binqian;Han Zhonghua

2008, (3): 583-595.

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Composite Structures for New Generation Large Commercial Jet
Abstract( 3037 )

Yang Naibin

2008, (3): 596-604.

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composite technology and large aircraft
Abstract( 2491 )

Chen Shaojie

2008, (3): 605-610.

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Interval Analysis for Stress Intensity Factors
Abstract( 2237 )

Wang Jun;Qiu Zhiping;Wang Xiaojun

2008, (3): 611-615.

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Dynamic Analysis of Aircraft Ground Steering and Braking Response
Abstract( 2621 )

Zhang Ming;Nie Hong

2008, (3): 616-621.

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Improved Zonal Safety Analysis Method
Abstract( 2943 )

Li Xiaolei;Tian Jin;Zhao Tingdi

2008, (3): 622-626.

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Crash Simulation of a Fuselage Section With Fuel Tank
Abstract( 2146 )

He Huan;Chen Guoping;Zhang Jiabin

2008, (3): 627-633.

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Equivalent Method of Using ESI for Corrosion Damage and Its Application
Abstract( 2686 )

Cao Dingguo;Ren Sanyuan;Wang Haowei

2008, (3): 634-639.

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Design of Composite Laminated Joint and Its Application in Large Aircrafts
Abstract( 3405 )

Cheng Jialin

2008, (3): 640-644.

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Convergence Analysis of Dynamic Condensation Methods
Abstract( 2467 )

Wang Xiaohong;Cao Lijuan;Liu Hui;Chen Huaihai

2008, (3): 645-650.

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Input-output Feedback Non-linearization Used in Design of Boom Air-refuelling Control System
Abstract( 2654 )

Hei Wenjing;An Gang;Lin Hao;Gao Fei

2008, (3): 651-656.

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The Research of Fuel Quantity Gauging Syncopation Step-size Choosing Based on Aircraft Fuel Tank Model Shape Feature
Abstract( 2628 )

Yang Pengtao;Niu Liang;Jiang Junchang

2008, (3): 657-663.

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A Structural Optimization Method for Aircraft Family
Abstract( 2710 )

Yong Mingpei;YU Xiongqing

2008, (3): 664-669.

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Numerical Study of Medium Stealth Scaledown Models for Airfoil Shape
Abstract( 2647 )

Sun Qin;Tian Wei

2008, (3): 670-675.

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Research on Electromagnetic Scattering Characteristics of Slits on Aircraft
Abstract( 2383 )

Huang Peilin;Liu Zhanhe

2008, (3): 675-680.

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Avionics and Autocontrol

Ideas for Developing Airborne Equipment for China’s Large Aircraft
Abstract( 2711 )

Feng Peide

2008, (3): 681-685.

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Research on Dissimilar Redundant Flight Control Computers of Large Civil Aircraft
Abstract( 2700 )

Qin Xudong;Chen Zongji;Li Weiqi

2008, (3): 686-694.

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A Gray Clustering Filtering Algorithm for Identifying False Alert in  Aircraft Longdistance Fault Diagnosis
Abstract( 4512 )

Geng Hong;Dong Jiankang

2008, (3): 695-700.

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One Generation of Material Technology, One Generation of Large Aircraft
Abstract( 2937 )

Cao Chunxiao

2008, (3): 701-706.

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Breaking Through the Common Technical Trend, Boeing Shows the Competition SuperiorityOnce Again
Abstract( 3334 )

Fan Ping;Fan Yuqing

2008, (3): 707-715.

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Exploration of Electromagnetic Riveting Application in Large Aircraft Manufacturing
Abstract( 2775 )

Cao Zengqiang

2008, (3): 716-720.

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Forming Technologies for Integral Panel
Abstract( 3333 )

Zeng Yuansong;Huang Xia

2008, (3): 721-727.

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Age Forming of Large Scale Integral Aircraft Wing Panel
Abstract( 2811 )

Wang Junbiao;Liu Zhongkai;Zhang Xianjie

2008, (3): 728-733.

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Automatic Assembly Technology for Large Aircraft
Abstract( 3389 )

Xu GuoKang

2008, (3): 734-740.

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Adhesive Property of Polyimide Adhesive
Abstract( 3095 )

Zhang Bin;Sun Mingming;Li Jian;Zhang Xugang;Zhang Milin;Li Jianhui;Wang Lei

2008, (3): 741-745.

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Electrochemical Impedance Varieties of Zinc Yellow Polypropylene Coated Aluminum  Alloy Used in Aircraft During the Accelerated Degradation Test
Abstract( 3203 )

Sun Zhihua;Zhang Ni;Cai Jianping;Liu Ming;Lu Feng

2008, (3): 746-751.

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Resin 3238 and Its Modification
Abstract( 2254 )

Shen Chao

2008, (3): 752-756.

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Research and Implementation of Method of Layout Design for Large Tooling in Aircraft Manufacture
Abstract( 3162 )

Pan Zhiyi;Huang Xiang;Li Yingguang

2008, (3): 757-762.

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Effects of Z-pin Inserting Parameters on X-Cor Sandwich Mechanical Property
Abstract( 2565 )

Zhang Zuoguang

2008, (3): 763-768.

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