1672-3147
2014 Issue 2
Aerodynamic and Infrared Radiation Characteristics Numerical Simulation on Single Expansion Ramp Nozzle within Aircraft
CHEN Zhu;,DENG Hong-wei;,SHAN Yong;,SHANG Shou-tang;,SHAO Wan-ren;
CHEN Zhu;,DENG Hong-wei;,SHAN Yong;,SHANG Shou-tang;,SHAO Wan-ren;
..............page:1-5
Discuss on Aeroengine Stealth Technology Research and Management
CAO MAO-guo;,DENG Hong-wei;,LI Feng;,SHANG Shou-tang;,TANG Zheng-fu;,YANG Sheng-nan;
CAO MAO-guo;,DENG Hong-wei;,LI Feng;,SHANG Shou-tang;,TANG Zheng-fu;,YANG Sheng-nan;
..............page:6-9,18
Analysis of Stealthy Shape Design Technology for Aeroengine Exhaust Nozzle
DENG Hong-wei;,JIA Dong-bing;,TANG Zheng-fu;,ZHAO Chun-sheng;
DENG Hong-wei;,JIA Dong-bing;,TANG Zheng-fu;,ZHAO Chun-sheng;
..............page:10-14,37
Thermal Stability of a Low Infrared Emissivity Coating
DING He-yan;,LIU Peng-rui;,WANG Zhi-yong;,XIAO Sheng-rong;,ZHANG Tong;
DING He-yan;,LIU Peng-rui;,WANG Zhi-yong;,XIAO Sheng-rong;,ZHANG Tong;
..............page:15-18
Mechanical Behaviors and Dynamic Characteristics of Turbofan Engine due to Fan Blade Off
HAO Yong;,HONG Jie;,LIANG Zhi-chao;,ZHANG Bo;
HAO Yong;,HONG Jie;,LIANG Zhi-chao;,ZHANG Bo;
..............page:19-23
Summary of Advanced Afterburner Design Technology
LIU Tao;,SUN Yu-chao;,ZHANG Xiao-chun;
LIU Tao;,SUN Yu-chao;,ZHANG Xiao-chun;
..............page:24-30,60
Numerical Simulation of Full Scale Unsteady Flow in High Pressure Turbine
LIU Dong-hua;,LUO Jian-qiao;,QI Lei;,SHAO Fei;
LIU Dong-hua;,LUO Jian-qiao;,QI Lei;,SHAO Fei;
..............page:31-37
Probability Analysis of Structure Stress and Deformation for Aeroengine Bladed Disk
BAI Bin;,BAI Guang-chen;,LI Xiao-ying;,TONG Xiao-chen;
BAI Bin;,BAI Guang-chen;,LI Xiao-ying;,TONG Xiao-chen;
..............page:38-46
A Design Method and Performance Research of Separately Exhaust System
CHEN Jun;,LI Yong-guo;,LIU Jian-jun;,WANG Wei;,ZHANG Jian-dong;
CHEN Jun;,LI Yong-guo;,LIU Jian-jun;,WANG Wei;,ZHANG Jian-dong;
..............page:47-50,69
Numerical Simulation on Interior Flow Field for a Gas Turbine Inlet System
LIU Chang-qing;,SUN Yong;,XU Xin;,ZHANG Ya-dong;
LIU Chang-qing;,SUN Yong;,XU Xin;,ZHANG Ya-dong;
..............page:51-55,75
Analysis and Design of Low Pressure Turbine Tip Clearance for High Bypass Ratio Turbofan Engine
HAO Yong;,HONG Jie;,LIU Bao-long;,ZHANG Da-yi;,ZHANG Qing;
HAO Yong;,HONG Jie;,LIU Bao-long;,ZHANG Da-yi;,ZHANG Qing;
..............page:56-60
Research on Design Technology of Planetary Gear System for Geared Turbofan Engine
HOU Ming-xi;,LI Jin-hua;,SHI Yan-yan;,XING Bin;,ZHANG Mao-qiang;
HOU Ming-xi;,LI Jin-hua;,SHI Yan-yan;,XING Bin;,ZHANG Mao-qiang;
..............page:61-64
Research on Bird Impact of Aeroengine First Stage Fan
JIANG Jia-yu;,MA Li;,XUE Qing-zeng;
JIANG Jia-yu;,MA Li;,XUE Qing-zeng;
..............page:65-69
A Mixture Solution Method Based on Variable Scale Method for Aeroengines State Variables Model
HUANG Jin-quan;,QIU Xiao-jie;,WANG Tie;,YANG Zheng-shan;
HUANG Jin-quan;,QIU Xiao-jie;,WANG Tie;,YANG Zheng-shan;
..............page:70-75
Effect of Different Swirl Cup on Combustion Performance in Revolving Streamline Vortex Combustor
LIU Guo-ku;,YANG Li-shan;,ZHANG Zhi-bo;,ZHENG Hong-tao;
LIU Guo-ku;,YANG Li-shan;,ZHANG Zhi-bo;,ZHENG Hong-tao;
..............page:76-80
Measures and Key Technologies for Improving Supportability of 4th Fighter Engine in USA
LIANG Chun-hua;,XU Qing-ze;
LIANG Chun-hua;,XU Qing-ze;
..............page:81-86
Difference Value Analysis of Dual Engines Performance Parameters on Aeroengine Fault Diagnosis
CHEN Jian;,DU Jun;,SHI Xiu-yu;
CHEN Jian;,DU Jun;,SHI Xiu-yu;
..............page:87-89,94
Construction of Combustor Test Database for Aeroengine
CHENG Ming;,LIN Hong-jun;,MA Hong-yu;
CHENG Ming;,LIN Hong-jun;,MA Hong-yu;
..............page:90-94
..............page:封2
..............page:封3