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System

Study of Flow Control of Inward Turning Inlet

WANG Wei-xing1,2,GU Qiang2,GUO Rong-wei2

2017, 38 (5): 961-967   

Study on Mode Transition Multi-Variable Control for Turbine-Based Combined Cycle Engine

NIE Ling-cong1,LI Yan1,2,DAI Dong-hong1,JIANG Wei-yu1,HOU Ying-dong1,WU Zhi-feng1

2017, 38 (5): 968-974   

Flow Characteristics of a Rectangular Low-Boom Supersonic Inlet

RAO Cai-yan,TAN Hui-jun,ZHANG Yue

2017, 38 (5): 975-982   

Analogy Between Effects of Attack Angle and Mach Number on Inlet Starting

GUO Shuai-tao1,LI Zhu-fei1,GAO Wen-zhi2,YANG Ji-ming1

2017, 38 (5): 983-991   

Characteristic Analysis of Muzzle Flow Fields Induced by Large Diameter Ultra-High Speed Balanced Gun

LI Zi-jie,CHEN Jian-wei,WANG Hao,WANG Jian

2017, 38 (5): 992-997   

Optimization Design of Hypersonic Inward Turning Inlet Based on SSPNS Algorithm

GAO Kun-peng,CHEN Bing,XU Xu

2017, 38 (5): 998-1007   

Study on Performance Impact of Boundary Layer Bleed on Curved Wall with Center Clapboard in Chamber

ZHAO Jian,FAN Xiao-qiang,TAO Yuan,LI Teng-ji

2017, 38 (5): 1008-1015   

Conversion and Application of Streamline-Characteristic Coordinate System Conversion in Supersonic Flows

SHI Chong-guang,LI Yi-qing,HAN Wei-qiang,YOU Yan-cheng

2017, 38 (5): 1016-1022   

Ship Propulsion

Experimental Investigation on Boundary Layer Transition Process in High-Lift Low-Pressure Turbines

LIANG Yun,LIU Huo-xing,ZOU Zheng-ping

2017, 38 (5): 1023-1029   

Effects of Actuation Parameters on Flow Separation Control in Compressor with Synthetic Jets

QIN Yong,LIU Hua-ping,WANG Ruo-yu,SONG Yan-ping,CHEN Fu

2017, 38 (5): 1030-1037   

Effects of Inlet Probe Support on Aerodynamic Performance of 1.5-Stage Compressor

YANG Rong-fei1,ZHAO Jian-tong1,XIANG Hong-hui2,GAO Jie2

2017, 38 (5): 1038-1046   

Close Loop Real Test of Improved Vaned Diffuser Ratio for Basic Stage

CHENG Chao1,2,QIN Guo-liang1,ZHANG Jia-zhong1,CHEN Dang-min2,LI Xin-hong2

2017, 38 (5): 1047-1054   

Effects of Asymmetry Wakes on Boundary Layer of Low Pressure Turbine Blade

QU Chun-gang1,SUN Shuang1,TONG Guo-xiang1,XIE Jiang2,FU Yu1,KONG Qing-guo3

2017, 38 (5): 1055-1064   

Effects of Hole Pitch on Characteristics of Improving Film Cooling by Sawtooth Slots

LI Guang-chao1,WU Zhuang1,LIU Yong-quan2,ZHANG Wei1,KOU Zhi-hai1,ZHAO Guo-chang1

2017, 38 (5): 1065-1072   

Effects of Fuel-Addition Distance and Fuel Ratio on Precombustion and Thermal Cracking in 2-Stage PDE

ZHU Xiao-bin1,CHEN Xin1,2,ZHANG Feng3,TAN Sheng1,HE Li-ming1

2017, 38 (5): 1073-1083   

Study on Model Modification and Particle Density in Sparse-Lagrangian Simulation

XU Dong,XIA Zhao-yang,YE Tao-hong

2017, 38 (5): 1084-1092   

Research on Thermo-Chemical Tabulation of Strained Laminar Premixed Flame

TANG Peng1,2,ZHANG Hong-da1,YE Tao-hong1,YU Zhou1

2017, 38 (5): 1093-1099   

Effects of Pressure Pulsation Upstream of Injector on Impinging Injector Atomization

YANG Shang-rong,YANG An-long,LI Long-fei,FEI Jun,ZHANG Feng

2017, 38 (5): 1100-1106   

Structure, Strength and Reliablity

Impact of Typical Operating Conditions on Creep Life Consumption for Aero Engine Turbine Blade

LI Ben-wei1,ZHAO Yong1,JIANG Ke-yi1,LI ZhaO2

2017, 38 (5): 1107-1114   

Dynamic Characteristics of One-Dimensional Feeding Pipe-Injector System Considering Fluid- Structure Interaction

XU Yun-fei,LI Feng,LI Long-fei,DENG Chang-hua,LIU Shang

2017, 38 (5): 1115-1122   

LCF Optimization of Single Crystal Superalloy Blade Considering Stress Concentration and Crystallographic Orientation

SUN Wan-chao

2017, 38 (5): 1123-1132   

Exploration of Schedules of Variable Geometry of Variable Cycle Engine with Double Bypass Duct Mode

LUO Guang-qi,GUAN Lei,ZENG Jian-chen,WU Tao,HU Shen-dao

2017, 38 (5): 1133-1139   

An Enhanced Spectral Kurtosis Methodforaero-Engine Gear Hub Fault Diagnosis

ZHONG Ye-pan,CHEN Wei,DU Wei,GONG Meng-lin

2017, 38 (5): 1140-1146   

Aero-Engine Vibration Fault Diagnosis Based on Supervised Manifold Learning

ZHANG Yun1,YANG Dong2,SI Yan-gang2,FANG Xu-meng2

2017, 38 (5): 1147-1154   

Intelligent Dual Response Surface Method for Reliability Sensitivity Analysis of Turbine Blisk

ZHANG Chun-yi1,SONG Lu-kai1,FEI Cheng-wei2,HAO Guang-ping1,LI Xue-qin3

2017, 38 (5): 1155-1164   

Study on Satellite Mass Moment Control for Fast Orbit Maneuver Using Solid Rocket Motor

LU Zheng-liang,ZHANG Xiang,YU Yong-jun,MO Qian-kun,LIAO Wen-he

2017, 38 (5): 1165-1172   

Material,Propellant and Fuel

Optimization Design of Nozzleless Booster Grain

HUANG Li-keng,YANG Yu-xin,HUO Dong-xing,MA Li-feng

2017, 38 (5): 1173-1179   

Numerical Model Solution and Analysis of Effect Factors of Boron Ignition and Combustion Behaviors

AO Wen1,QUAN En2

2017, 38 (5): 1180-1187   

Electric Propulsion and Other Advanced Propulsion

Selection Method of Key Parameters for Wave Drag Reduction by High Frequency Laser Energy

WANG Dian-kai,QING Ze-xu,LI Qian,FANG Juan

2017, 38 (5): 1188-1193   

Experimental Study on Acoustic Behavior of Dual-Tube Pulse Detonation Engine in Near Field

HUANG Xiao-long,WENG Chun-sheng,LI Ning,XU Gui-yang

2017, 38 (5): 1194-1200