1673-1220
2003 Issue 4
THE DESCENDIBLITY COMBINATION ARITHMETIC AND THE APPLICATION IN HELICOPTER TIPTOP LAYER DESIGN
duan guo he ; fang ming yun
duan guo he ; fang ming yun
..............page:6-10
guo wai zhi sheng ji ji zai lei da de xian zhuang yu fa zhan qu shi
zheng min ; zhou zuo ; zhao yu jie
zheng min ; zhou zuo ; zhao yu jie
..............page:42-48
THE APPLICATION ENVIRONMENT OF CONCURRENT ENGINEERING IN HELICOPTER DESIGN
huang lan ; zheng wen xin ; huang zuo ; peng yong ; fu xiao bing
huang lan ; zheng wen xin ; huang zuo ; peng yong ; fu xiao bing
..............page:1-5
zhi sheng ji fa zhan gai shu
yu zhang
yu zhang
..............page:35-41
ANALYSIS ON STRUCTURE AND MAINTENANCE FEATURES OF Mi- 171
hou sheng li ; ao liang
hou sheng li ; ao liang
..............page:32-34
NON-DESTRUCTIVE TESTING METHOD FOR DAMAGE-DETECTION BASED ON THE X-RAY CCD IMAGE AND WAVELET ANALYSIS
jiang yun fei ; liu wen bo
jiang yun fei ; liu wen bo
..............page:23-26
THE FINITE ELEMENT ANALYSIS ON VIBRATION ACCELERATION RESPONSE OF HELICOPTER FUSELAGE
han pu xiang ; yu gui chuan ; ling ai min ; li wu zhou
han pu xiang ; yu gui chuan ; ling ai min ; li wu zhou
..............page:11-14
ba609 min yong qing zhuan xuan yi ji
shao ming
shao ming
..............page:49-52
THE ELECTROMAGNETIC COMPATIBILITY ANALYSIS ON THE INTERFERENCE OF THE DIPPING SONAR DOME WITH FLOATING EARTH DESIGN TO THE AVIONICS EQUIPMENT
qu ye pin ; ye zhou ying ; jia chang sheng
qu ye pin ; ye zhou ying ; jia chang sheng
..............page:20-22
..............page:27-31
TOP DESIGN TECHNIQUE OF FLY-BY-WIRE CONTROL SYSTEM FOR HELICOPTER
lai shui qing ; li lin hua
lai shui qing ; li lin hua
..............page:15-19