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Aeroengine
1672-3147
2002 Issue 4
"kun lun " fa dong ji ( tu pian )
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page:封三
"kun lun " fa dong ji fu zong she ji shi yang shi jie zhuan fang
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page:封二
tech56 ji shu ji hua de gao ya ya qi ji ji shu
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page:43
tech56 ji shu ji hua de wo lun ji shu
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page:11
tech56 ji shu ji hua de fa zhan
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page:21
mei guo chao gao xiao fa dong ji ji shu ji hua
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page:58
China Zhuhai Air Show Report
wu wen sheng
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page:47-47
DERA Core Compressor Demostration Program
jiang hao xing
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page:56-58
Investigation of Plasma Jet Ignition in Aircraft Engine
jin bao lin ; zheng yong cheng
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page:51-55
Robust Controller Design in Flight Control Uncertainty Svstem with Vectoring Thrust
chen hua rong ; wang zuo ; xing zhi qiang
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page:48-50,55
Design of LQG/LTR Multivariable Feedback Controller
guo ying qing ; wu dan ; zhang hua
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page:44-47
Investigation of Combustion Liner Wall Cooling in Gas Turbine Combustor
zuo yu zuo ; zhang bao cheng
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page:38-43
Fuzzy Decision for Design Values of Aeroengine Reliability
zhao de zi ; wang hou zuo
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page:33-37
Elimination of Aero Engine Augmenter Buzz
li yu tong ; zhang xiao xian
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page:29-32
Effect of Distortion on Aeroengine Stability
tian ning ; chen jin guo ; zhang en he
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page:25-28,37
High Energy X-Ray Instrumentation System for Aeroengine Test
bai ying zuo
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page:22-24,32
Experimental Investigation of Rotor-to-Casing Rubbing Fault
gao yan lei ; li yong ; wang de you
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page:16-21
Design of Aeroengine Life Monitor System Based on Flight Data
chen yong gang ; ni shi hong ; huang zhi yu
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page:12-15
Design Concept and Application of Integrated Flow Pattern of Bowed, Twisted and Swept Blade and Optimized Flow Field Structure
feng guo tai ; wang song tao ; gu zhong hua ; wang zhong qi
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page:5-11
Development of Side-Mounted, All-Time and Two-Phase Ignition System for Afterburner
zhang xiao chun ; fu zao qun ; lu fei
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page:1-4,15