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Aircraft Design
1673-4599
2002 Issue 2
DISCUSS THE AUDITOR'S QUALITY WITHIN THE QUALITY SYSTEM
chen lei ; yan shi guang
..............page:78-80
STUDY OF CHARACTERISTIC OF 1Cr18Ni10Ti STAINLESS STEEL AND PIPE
deng zhong ; kong fan ya
..............page:66-72
THE APPLICATION STUDY OF THE NEW TYPE TITANIUM TB8
yu dong mei
..............page:57-65
THE RESEARCH OF NiTiNb SHAPE MEMORY ALLOY TUBE COUPLING
jing lv lu ; guan de fu ; fan li wei
..............page:52-56
OPTIMAL DESIGN OF ON-STATE RESISTANCE FOR VDMOSFET
gao ya jun
..............page:48-51
THE MODEL MANAGEMENT SYSTEM OF FLIGHT CONTROL
tang yong zhe ; zhu zhi ping
..............page:34-38
APPLICATION OF ADAPTIVE NONLINEAR THEORY IN THE DESIGN OF A HELICOPTER FCS
xu chun chun ; wu wen hai ; geng chang mao
..............page:30-33
FATIGUE LIFE ANALYSIS FOR THE MAIN SPAR OF A A/C WING STRUCTURE
li yong gang ; zhu pei lin
..............page:25-29
DESIGN METHOD OF DIFFUSE DUCT OF A CARET INLET
zhang ling ling
..............page:18-20
AIRCRAFT SHORT-PERIOD MOTION PARAMETER IDENTIFICATION USING NEURAL NETWORK
li ai jun ; liu hui ying ; zhang wei guo
..............page:11-13
LOAD CAPABILITY OF COMPOSITE PLATE WITH ADHESIVE PATCH
chen hao ran ; cao ning yuan ; cheng wan zhi
..............page:1-5