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25 May 2009, Volume 30 Issue 5

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25 May 2009, Volume 30 Issue 5

论文

Influence of Crosswind Speeds on Aircraft Wake Vortex Movement
Abstract( 3237 )

Zhou Bin;Wang Xuesong;Wang Tao;Liu Junkai

2009, (5): 773-779.

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Numerical Simulation on Flowfield of Rotor in Ground Effect Based on Unstructured Embedded Grid Method
Abstract( 3194 )

Ye Liang;Zhao Qijun;Xu Guohua

2009, (5): 780-786.

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On-line Measurement and Stall Control by DSP in Singlestage Axial Compressor
Abstract( 3485 )

Li Lin;Nie Chaoqun

2009, (5): 787-793.

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3D Numerical Simulation of the Influence of Fuel Equivalence Ratio on  Single Cavity Supersonic Combustor Flow
Abstract( 3380 )

Chen Siyuan;Xu Xu

2009, (5): 794-799.

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Effect of the Control Style of a Stratospheric Airship on Its Floating Performance
Abstract( 3124 )

Shi Hong;Song Baoyin;Zhou Lei;Yao Qiuping

2009, (5): 800-805.

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Lateral Inject Active Vortex Control Based on Low Aspect Ratio Flying Wing
Abstract( 2960 )

Kong Yinan;Wang Lixin;Wang Guangxue;Hong Junwu

2009, (5): 806-811.

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Film Cooling Characteristics of Converging-xpanding Hole with Transient Liquid Crystal Measurement Technique
Abstract( 3179 )

Liu Cunliang;Zhu Huiren;Bai Jiangtao;Xu Duchun

2009, (5): 812-818.

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Characteristics of Icing in High Pressure Pneumatic Relief Valve with Slide Pilot
Abstract( 3059 )

Xu Zhipeng;Wang Xuanyin;Luo Yuxi

2009, (5): 819-824.

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Flow Separation and Control in Large Meridional Expansion Turbine
Abstract( 2624 )

Tang Hongfei;Yan Peigang;Huang Hongyan;Han Wanjin

2009, (5): 825-831.

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A New Aerodynamic Configuration of UAV with Variable Forward-swept Wing
Abstract( 3538 )

Liu Wenfa;Wang Xu;Mi Kang

2009, (5): 832-836.

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Remote Sensing of Aircraft Engine Exhausts Using FTIR-emission-spectroscopy
Abstract( 3288 )

Xia Qing;Zuo Hongfu;Xu Juan

2009, (5): 837-841.

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Convergence Characteristics of Preconditioned Euler Equations at Low Mach Numbers
Abstract( 2968 )

Liu Chen;Wang Jiangfeng;Wu Yizhao

2009, (5): 842-848.

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Nonlinear Optimal Control of Aircraft Arresting Process
Abstract( 2931 )

Zhang Shusen;Jin Dongping

2009, (5): 849-854.

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Evaluation of Missile Guidance Precision Based on Hybrid Prior Distribution
Abstract( 2771 )

Yang Huabo;Cai Hong;Zhang Shifeng

2009, (5): 855-860.

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Probabilistic Interval Approach for Determining the Demand of Aviation Spares
Abstract( 2958 )

Qiu Zhiping;Ni Zao

2009, (5): 861-866.

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Properties of Stitched Composite Laminates—Fatigue Performance of Composite Laminates with an Open-hole
Abstract( 3142 )

Cheng Xiaoquan;Zou Jian;Zhang Jikui;Li Zhengneng

2009, (5): 867-871.

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Fuzzy Reliability Analysis and Application of Structural Systems with Fuzzy Variables as Distribution Parameters
Abstract( 2585 )

Ni Zao;Qiu Zhiping

2009, (5): 872-878.

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Finite Element Algorithm of One-dimensional Damage Model Based on Nonlocal Theory
Abstract( 3085 )

Fu Li;Du Xingwen

2009, (5): 879-885.

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论文

Fuzzy Reliability Analysis Based on Probability Density Function Equivalent
Abstract( 2958 )

An Hai;An Weiguang;Zhou Ling

2009, (5): 886-894.

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Analysis System of Stability and Strength for Airframe Composite Stiffened Plate/Shell
Abstract( 3151 )

Lu Wenshu;Ma Yuanchun;Liang Wei;Lu Zixing

2009, (5): 895-900.

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Testability Verification Method Based on Data Evaluation in Development Phase
Abstract( 3063 )

Shi Junyou;Tian Zhong

2009, (5): 901-905.

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Study of Love Wave Aircraft Ice Sensor
Abstract( 2399 )

Jiang Cheng;Ni Shihong;Li Honglang;He Shitang;Zhang Zonglin

2009, (5): 906-911.

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Experimental Research on Scattering Characteristics of Bolt/Rivet Objects
Abstract( 2661 )

Huang Peilin;Liu Zhanhe

2009, (5): 912-918.

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Quantitative Forecast of Support Activity Centered Equipment Support Resources
Abstract( 2550 )

Guo Linhan;Kang Rui;Wen Jia

2009, (5): 919-924.

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Adaptive Multi-parameter Prediction Model Based on Grey Theory
Abstract( 3021 )

Guo Yangming;Jiang Hongmei;Zhai Zhengjun

2009, (5): 925-931.

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A Clutter Suppression Method Based on Angle-Doppler Compensation for Airborne Radar with Uniform Circular Array Antennas
Abstract( 2648 )

Zhao Jun;Zhu Zhaoda

2009, (5): 932-937.

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Trust Software Technology in Integrated Avionics Systems
Abstract( 3110 )

Shen Yulong;Cui Xining;Ma Jianfeng;Niu Wensheng;

2009, (5): 938-945.

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Tolerance Design Method Based on Maximum Tolerance Region
Abstract( 3161 )

Guo Jianbin;Tan Xinxin;Sun Yufeng;Zeng Shengkui

2009, (5): 946-951.

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Selective-disassembly Sequence Planning Based on Improved Genetic Algorithm
Abstract( 2895 )

Wu Hao;Zuo Hongfu

2009, (5): 952-958.

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Variant Design Method for Assembly Tooling Design Based on  Aircraft Product Structure Change
Abstract( 2853 )

Pan Zhiyi;Huang Xiang;Li Yingguang

2009, (5): 959-965.

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Experimental Research on IPMC Material Tensile Samples
Abstract( 2822 )

An Yi;Xiong Ke;Gu Na

2009, (5): 966-971.

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