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25 December 2003, Volume 24 Issue 6

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25 December 2003, Volume 24 Issue 6

论文

Comparison of Neural Network Model and Freguency Domain Quasi-Linear Model for Human Pilots
Abstract( 2088 )

TAN Wen-qian;QU Xiang-ju;WANG Wei-jun

2003, (6): 481-485.

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Optimilization of Bump Device Geometry Allocation Based on MAV Wing Shape Change
Abstract( 2098 )

ZENG Qing-hua;HE Lie-tang

2003, (6): 486-490.

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A Comparison of Two Turbulence Models on Computation of Three-Dimensional Separated Flow Around a Prolate Spheroid
Abstract( 2170 )

ZHU Cheng-min;XIN Ding-ding;ZHUANG Feng-gan

2003, (6): 491-494.

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Topological Analysis on the Effects of Unsteady Aerodynamics on Motion of Aircraft
Abstract( 2230 )

LIANG Su-nan;ZHANG Shu-guang

2003, (6): 495-498.

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Aircraft Referenced Flight Path Planning by Using Adaptive Genetic Algorithms
Abstract( 2305 )

HE Pei;QU Xiang ju;WU Zhe

2003, (6): 499-502.

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Experimental Study of the Evolutionary Process of the Flowfield Around Slender Body at High Angle of Attack
Abstract( 3329 )

LIU Pei-qing;SHAO Yan-feng;DENG Xue-ying;MA Yu

2003, (6): 503-506.

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Solution Methods of Inherent Characteristics of Plane Beam with Arbitrary Boundary Conditions
Abstract( 2031 )

XIE Wen-jian;XING Yu-feng;ZHU De-chao

2003, (6): 507-511.

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Approach to the Radiation of Burned Gas in Finite Element Analysis of Heat Transfer and Its Application in the Analysis of Temperature of Aircraft Structure
Abstract( 2657 )

XU Rang-shu;ZHANG Bao-cheng;NIU Ling;FU Li-xin

2003, (6): 512-516.

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Parameters Study at Touchdown Instant of the Nose Undercarriage of Fighter Airplane
Abstract( 2491 )

SHI Hai-wen;YANG Shu-xun;ZHANG Da-qian;FU Yong-hong

2003, (6): 517-520.

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Aeroelastic Analysis of a Two-Dimensional Airfoil with Control Surface Freeplay Nonlinearity
Abstract( 2073 )

ZHAO Yong-hui;HU Hai-yan

2003, (6): 521-525.

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Modal Parameters Identification of an Aircraft under Flutter Test Flying
Abstract( 2209 )

CHEN Kui-fu;JIAO Qun-ying

2003, (6): 526-530.

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Numerical Simulation of the Transient Response of Blade due to Bird Impact
Abstract( 2172 )

CHEN Wei;GUAN Yu-pu;GAO De-ping

2003, (6): 531-533.

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State Analysis Approach of Random Fatigue Reliability Prediction
Abstract( 2057 )

LIN Wen-qiang;XIE Li-yang

2003, (6): 534-536.

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A Modified PGA ML Phase Estimation Method
Abstract( 2222 )

Zhong Rui;Mao Shi-yi

2003, (6): 537-540.

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Model and Control Law of CMG Active Magnetic Bearing Rotor
Abstract( 2173 )

YU Wen-bo;LUAN Sheng;FANG Jian-cheng

2003, (6): 541-545.

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Research on a Novel Aircraft Static Inverter
Abstract( 2356 )

XIE Shao-jun;CHEN Wan;LI Fei

2003, (6): 546-550.

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Application of Wavelet Interpolation in Ultra-Wide Band Airborne SAR Imaging
Abstract( 2225 )

GUO Han wei;WANG Yan;LIANG Dian nong;HUANG Xiao tao

2003, (6): 551-554.

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Nonlinear Correction of Terminal Guidance Signal for an Antiship Missile
Abstract( 2339 )

WU Sen-tang;JIANG Zhi-chao;ZHANG Miao

2003, (6): 555-558.

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A Modified DS Evidence Combination Strategy
Abstract( 2759 )

He Bing;Hu Hong-li

2003, (6): 559-562.

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Optimization of Cathode Feed Direction in Electrochemical Machining of Turbine Blades
Abstract( 1851 )

LI Zhi-yong;ZHU Di;WANG Lei

2003, (6): 563-567.

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Effect of Mechanical Alloying on Synthesizing of Laves Phase Cr_2Nb by Solid Phase Thermal Reaction
Abstract( 1936 )

LU Shi-qiang;HUANG Bai-yun;HE Yue-hui

2003, (6): 568-572.

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Vertex Clustering-Based Algorithm for Simplification of Polyhedral Model
Abstract( 1998 )

WU Bo;SHI Fa zhong

2003, (6): 573-576.

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