1001-4055
2004 Issue 4
Application of PLIF in research on supersonic combustion
li mai liang ; zhou jin ; geng hui ; di zhen chen
li mai liang ; zhou jin ; geng hui ; di zhen chen
..............page:381-384
Flow field analysis on the characteristic of a high load compressor fan
yuan wei ; lu ya jun ; zhou sheng
yuan wei ; lu ya jun ; zhou sheng
..............page:377-380
Preparation and characterization of composite particles of Al/ammonium perchlorate
ma zhen ye ; li feng sheng ; chen ai si ; song hong chang
ma zhen ye ; li feng sheng ; chen ai si ; song hong chang
..............page:373-376
Effect of nano aluminum and nickel powders on the combustion properties of composite propellant
jiang zhi ; li shu fen ; zhao feng qi ; liu zi ru ; yin cui mei ; luo yang ; li shang wen
jiang zhi ; li shu fen ; zhao feng qi ; liu zi ru ; yin cui mei ; luo yang ; li shang wen
..............page:368-372
Influence of POM(acetal copolymer) on the thermal behavior and combustion properties of smokeless XLDB propellant
zhang wei ; fan xue zhong ; fan hong jie ; hu rong zu ; zhao feng qi
zhang wei ; fan xue zhong ; fan hong jie ; hu rong zu ; zhao feng qi
..............page:363-367
Experimental investigation on multiple-start in hybrid motor
yang wei ; zhang hai tao ; mao li wen ; dai zu ming
yang wei ; zhang hai tao ; mao li wen ; dai zu ming
..............page:360-362
Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade
sun yang ; lu jian ; zheng yan ; hong jie ; cao hang ; zhang rui hu
sun yang ; lu jian ; zheng yan ; hong jie ; cao hang ; zhang rui hu
..............page:357-359
Method for diagnosis the fault in parts of nonlinear system
song zhi ping ; wei rui xuan ; han chong zhao
song zhi ping ; wei rui xuan ; han chong zhao
..............page:354-356
Experimental investigation on internal flow in rectangular isolator under non-uniform supersonic flow
wang cheng peng ; zhang yuan ; jin zhi guang ; li nian
wang cheng peng ; zhang yuan ; jin zhi guang ; li nian
..............page:349-353
Quasi-3D calculation of influence of inlet distortion on axial flow compressor performance
wang yong ming ; hu jun ; deng yan
wang yong ming ; hu jun ; deng yan
..............page:343-348
Effect of blade sweeping-curving on the endwall flow field of compressor cascade
song yan ping ; liu zhen de ; zhao gui jie ; wang zhong qi
song yan ping ; liu zhen de ; zhao gui jie ; wang zhong qi
..............page:338-342
Effects of front guide blade on performance and vortices structure in two turbine low pressure guide vanes
an bai tao ; han wan jin ; wang song tao ; wang zhong qi
an bai tao ; han wan jin ; wang song tao ; wang zhong qi
..............page:333-337
Flow behavior analysis in a radial inflow turbine for very small aero-engines
wen quan ; liang de wang
wen quan ; liang de wang
..............page:329-332
Numerical investigation of the effect of hub leakage flow on transonic compressor rotor
ning fang fei ; xu li ping
ning fang fei ; xu li ping
..............page:325-328,342
Numerical computation and examination of a lobed mixer-ejector
dan yong ; zhang jing zhou
dan yong ; zhang jing zhou
..............page:320-324
Structural design analysis for platelet transpiration cooling section at throat of thrust chamber
yang wei hua ; cheng hui er ; wang ping yang ; wu li jun
yang wei hua ; cheng hui er ; wang ping yang ; wu li jun
..............page:316-319
Effect of unsteady wake on linear cascade film cooling efficiency
jiang xue hui ; zhao xiao lu
jiang xue hui ; zhao xiao lu
..............page:311-315
Numerical study on heat transfer and pressure drop in pin-fin channels with lateral flow ejection
zhang li ; liu song ling
zhang li ; liu song ling
..............page:307-310
A new model for film cooling effectiveness computation on blade surface in a turbine cascade
xiang an ding ; liu song ling ; zhu hui ren
xiang an ding ; liu song ling ; zhu hui ren
..............page:303-306
Heat transfer characteristics in round to square nozzle
li jun wei ; liu yu
li jun wei ; liu yu
..............page:298-302,315
Numerical simulation of reacting fuel-rich flow field laden with boron particle in the ramjet combustor
wu yuan ; tian wei ping ; le fa ren ; yu zhen yong
wu yuan ; tian wei ping ; le fa ren ; yu zhen yong
..............page:294-297
Three-dimensional numerical and experimental investigationon supersonic secondary combustion
ma chao zuo ; xu xu ; liu ming zuo ; cai guo zuo
ma chao zuo ; xu xu ; liu ming zuo ; cai guo zuo
..............page:289-293