1001-4055
2004 Issue 3
Fiber bridge analysis in filament winding of concave revolution surface and its application
han zhen yu ; fu hong ya ; fu yun zhong ; wang yong zhang
han zhen yu ; fu hong ya ; fu yun zhong ; wang yong zhang
..............page:286-288
Research of single-feeding recirculation in cryogenic propellant transfer system
zhang liang ; lin wen sheng ; lu xue sheng ; gu an zhong
zhang liang ; lin wen sheng ; lu xue sheng ; gu an zhong
..............page:282-285
Method on predicting burning surface temperature of solid propellant
song hong chang ; wang dai
song hong chang ; wang dai
..............page:278-281
Design the sample of the debond propagation in burning propellant
yang jian hong ; hou gen liang ; liu chao feng ; cheng shu ; he guo qiang ; lv qiu juan ; yue ying juan
yang jian hong ; hou gen liang ; liu chao feng ; cheng shu ; he guo qiang ; lv qiu juan ; yue ying juan
..............page:274-277,281
Synthesis and characterization of thermoplastic polyurethane elastomer for propellants
he ji yu ; tan hui min
he ji yu ; tan hui min
..............page:271-273
Investigation of aerodynamic design of low pressure turbine at low reynolds number conditions
li wei ; zou zheng ping
li wei ; zou zheng ping
..............page:219-223
Research on stalling recoverability of an axial-flow compressor with treated casing
wu yan hui ; chu wu li ; liu zhi wei
wu yan hui ; chu wu li ; liu zhi wei
..............page:215-218
Influence of positive curving on blade surface flow of compressor cascade
wang hui she ; yuan xin ; zhong jing jun ; wang zhong qi
wang hui she ; yuan xin ; zhong jing jun ; wang zhong qi
..............page:210-214
Two phase flow combustion modeling of secondary combustion chamber in a unchoked ducted rocket
hu jian xin ; xia zhi xun ; liu jun ; luo zhen bing ; zuo wan bo ; zhao jian min
hu jian xin ; xia zhi xun ; liu jun ; luo zhen bing ; zuo wan bo ; zhao jian min
..............page:193-195,240
Study of experimental method for ablation of insulator of SRM with high acceleration (Ⅱ) Convergent tube experimental method
li jiang ; he guo qiang ; chen jian ; liu yang ; lou yong chun
li jiang ; he guo qiang ; chen jian ; liu yang ; lou yong chun
..............page:196-198
Numerical simulation of synthetic jet flow field and parameter analysis of actuator
luo zhen bing ; xia zhi xun ; hu jian xin ; zhao jian min ; zuo wan bo ; wang de quan
luo zhen bing ; xia zhi xun ; hu jian xin ; zhao jian min ; zuo wan bo ; wang de quan
..............page:199-205
Influence of injection angle on the aerodynamic aspects of endwall film-cooling in a turbine cascade
liu gao wen ; liu song ling
liu gao wen ; liu song ling
..............page:206-209
Experimental investigation for coaxial hydrogen/oxygen resonance ignitor
yu nan jia ; zhang guo zhou ; song ya na ; ma bin ; tong xiao yan
yu nan jia ; zhang guo zhou ; song ya na ; ma bin ; tong xiao yan
..............page:267-270
Numerical simulation for the flow fields within microwave plasma thruster nozzle
xiao ying chao ; tang hai bin ; yang zuo ; mao gen wang ; wang chang hui
xiao ying chao ; tang hai bin ; yang zuo ; mao gen wang ; wang chang hui
..............page:263-266
Development of microwave source of microwave plasma thruster operating under vacuum condition
yang zuo ; he hong qing ; mao gen wang ; wei kun ; tang jin lan ; song jun ; chen jun
yang zuo ; he hong qing ; mao gen wang ; wei kun ; tang jin lan ; song jun ; chen jun
..............page:259-262
Effects of plug sidewall on linear plug nozzles performance
li jun wei ; liu yu ; wang chang hui
li jun wei ; liu yu ; wang chang hui
..............page:252-258
Theoretical computation for microwave plasma thruster with cylindrical resonant cavity
tang jin lan ; he hong qing ; mao gen wang ; han xian wei ; yang zuo
tang jin lan ; he hong qing ; mao gen wang ; han xian wei ; yang zuo
..............page:246-251
Net thrust prediction of multi-cycle pulse detonation engine
li jian zhong ; wang jia zuo ; fan yu xin ; zhang jing guo
li jian zhong ; wang jia zuo ; fan yu xin ; zhang jing guo
..............page:241-245
Application of genetic algorithm in aeroengine nonlinear mathematical models
su san mai ; lian xiao chun
su san mai ; lian xiao chun
..............page:237-240
Multivariable optimal acceleration control of turbofan engine based on FSQP algorithm
qi xue feng ; fan ding ; chen yao chu ; li wei gang
qi xue feng ; fan ding ; chen yao chu ; li wei gang
..............page:233-236
Predictive control design on power pack of cruise missile
sun ming zuo ; wang jian ; xue li hua
sun ming zuo ; wang jian ; xue li hua
..............page:230-232
Concept of a two-dimensional supersonic/hypersonic inlet with a non-conventional compression wall
jin zhi guang ; zhang yuan
jin zhi guang ; zhang yuan
..............page:226-229
Experimental investigation of flow vectoring by using zero-mass synthetic jets actuator
zhang yuan ; li nian ; dong ; lu zhen qiu
zhang yuan ; li nian ; dong ; lu zhen qiu
..............page:224-225,236