1673-4599
2002 Issue 3
LINEAR DESIGN AND SIMULATION FOR INTEGRATED FLIGHT/FIRE CONTROL SYSTEM
fan yi ; shen gong zuo
fan yi ; shen gong zuo
..............page:1-5
THE NUMERICAL SIMULATION OF COMPOSITE LAMINATES TENSILE DESTRUCTION BASED ON THE PROGRESSIVE FAILURE METHOD
sun zhong kai ; li shu ; zhang zuo ning
sun zhong kai ; li shu ; zhang zuo ning
..............page:6-8
A EQUIVALENT METHOD TO SOLVE THE AXIS–SYMMETRY PROBLEM
he li jun ; lv guo zhi
he li jun ; lv guo zhi
..............page:9-11
CORROSION FAILURE ANALYSIS OF CERTAIN AIRCRAFT STRUCTURE
chen yue liang ; yu ji zhen
chen yue liang ; yu ji zhen
..............page:12-16,27
EXPONENTIAL FUNCTION METHOD ON NONLINEAR PROGRAMMING
deng yang chen ; zhang zuo ning ; zuo zheng neng
deng yang chen ; zhang zuo ning ; zuo zheng neng
..............page:17-23
THE IMPROVEMENT OF MEASUREMENT METHOD FOR TYER HORIZONTAL LOAD IN DROP-TEST
shi hai wen ; yang shu xun ; fu yong hong ; zhang da qian
shi hai wen ; yang shu xun ; fu yong hong ; zhang da qian
..............page:24-27
EXISTING TOOLING BASED AIRCRAFT CONTOUR GENERATION MATHEMATICAL MODEL DEVELEPMENT
yang shi fu ; jiang
yang shi fu ; jiang
..............page:28-30
AIRCRAFT FUEL DENSITY MEASUREMENT BASED ON RADIATION ATTENUATION LAW
li zuo ; lv jun fang
li zuo ; lv jun fang
..............page:31-34
RESEARCH ON REDUNDANT TECHNIQUE OF FBL FLIGHT CONTROL SYSTEM
duan hai bin ; gong hua jun ; yang yi dong
duan hai bin ; gong hua jun ; yang yi dong
..............page:35-39,70
DESIGN OF A INTEGRATED FIRE/FLIGHT CONTROL SYSTEM
yu jian li ; wu wen hai ; jin xian kun
yu jian li ; wu wen hai ; jin xian kun
..............page:40-46
THE CONSTRUCTION OF THE ENTEROPRISE SECURE NETWORK
ding san jun
ding san jun
..............page:47-48,78
..............page:49-52
..............page:53-57
DESIGN AND INSTALLATION OF FILTERS
wang tian shun
wang tian shun
..............page:58-63
THE INTEGRAL PROPERTY OF THE TRANSPARENCY IS IMPORTANT WHEN SELECTING MATERIAL FOR ITS STRENGTH DESIGN
zuo xiang fa ; wang jia ying
zuo xiang fa ; wang jia ying
..............page:64-66
THE FINITE ELEMENT MODEL BUILD UP AND THE STABILITY ANALYSIS OF ×× AIRCRAFT WINDSHIELD
wang jia ying ; zuo xiang fa
wang jia ying ; zuo xiang fa
..............page:67-70
NEUROFUZZY BASED CONTROL TO ACCELERATING PROCESS OF TURBOFAN AEROENGINE
ma hui min ; fu hong ying ; fan si qi
ma hui min ; fu hong ying ; fan si qi
..............page:71-74
..............page:75-78
The Discussion of Unmanned Aircraft
xu zheng rong
xu zheng rong
..............page:79-80