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Aircraft Design
1673-4599
2010 Issue 1
Wing Structural Weight Analysis of Transport Aircraft with Maneuvering Load Alleviation Function
ma jie xiang
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page:38-42,54
Zonal Safety Analysis Evaluation Based on Set Pair Analysis
yan chun yan ; zhu wen jie ; sun you chao ; che cheng
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page:47-50
Analysis of a Fighter\'s Lateral and Directional Flying Qualities
dai gui cheng ; wei jin peng
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page:16-19
The Model Analysis in the Application of the Piezoelectric Actuator
jia li jie ; li min
..............
page:20-24
Critical Technologies of Simulation Analysis on Thermal-Loads of the Radome in Flight
zhang juan ; tian zhong qiang ; gao xing shan ; yue zhu feng
..............
page:31-33,37
Research of Temperature Control Technology in Cabin Fatigue Test
xu chang jun ; liu dao qing ; zhou bao quan
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page:51-54
The Optimization Design of the Wing with Low Detectable Structure
li hong xin ; shen hai jun
..............
page:5-8
Standardization Management for Technical Document
dai hong xia
..............
page:77-80
The Design and Simulation of Jerusalem FSS
an zhao wei ; wang ming zuo ; zhao ping ; hong tie shan ; li qing bo
..............
page:55-59
Mechanical Design and Research of Trailing Edge Flap for Civil Aircraft
yi zhi sheng ; he jing wu
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page:43-46
The Main Technology Approach that Foreign Aircraft Life Extension Obtained Important Develop——The Durability Repair that Confer Afresh Life of Aircraft
huang ji zuo ; sui fu cheng
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page:1-4
Research of the Advanced Aircraft 270VHDC Power System Demonstration Software Based on LabVIEW
chen wei hua ; tie cheng ; dai zhen dong ; zhang shu juan ; yang shan shui
..............
page:60-63
The Use of DATACOM Method for Flying Wing UAV Modeling
wu fan ; jiang chang sheng
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page:9-15
The Service Feasibility Study of Infrared Missile for Single-to-Multiple Attack
zuo xu ; feng bai run ; zhang tian yu
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page:72-76
Effect of Plastic Zone Around Crack-Tip and Its Criterion in Fracture Analysis
zhang xian yu ; fu chang an
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page:34-37
The Calculation of Anti-Radiation Missile Launching Area
zhou shuai ; zuo xu ; feng bai run
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page:69-71
Study on Determination of Wing Load by Engineering Methods
liu shu yuan
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page:25-30
Quantitative Analysis of Fault Tree Application in Draw and PutSystem of Undercarriage of the Ship-Based Helicopter
zhang feng ; lu kun ; xu ting xue
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page:64-68