An Experimental Study on Flow Structure of a Supersonic Mixing Layer Influenced by Forced Vibration
ZHANG Dong-dong;TAN Jian-guo;LV Liang;Science and Technology on Scramjet Laboratory;National University of Defense Technology;

..............page:601-607

Experimental Study of Transition Mechanism of Mach Reflection of Detonation Wave
LIU Jie;DU Zhong-hua;School of Mechanical Engineering;Nanjing University of Science and Technology;

..............page:608-616

Zero-Fuel Internal Flow Force Test for Circular Cross Section Scramjet Engine
WANG Ze-jiang;TANG Xiao-wei;SONG Wen-ping;ZHANG Yong;School of Aeronautics;Northwestern Polytechnical University;China Aerodynamic Research and Development Center;

..............page:617-623

An Inverse Method for Supersonic Flowfield with Given Downstream Boundary
HAN Wei-qiang;ZHU Cheng-xiang;YOU Yan-cheng;LI Yi-qing;School of Aerospace Engineering;Xiamen University;

..............page:624-631

Application of Non-Linear Harmonic in Turbomarchinery 3D Flow Field Unsteady Simulation
YAO Xiao-jiang;DONG Jing-xin;SHANG Jie;ZHU Zhao;SUI Jun-you;Department of Precison Instrument;Tsinghua University;Oilfield Technology Group;China Oilfield Services Company Limited;NUMECA China;

..............page:632-639

Effects of Twin Swirl on Performance and Stability of Compressor Rotor
TU Bao-feng;HU Jun;ZHANG Kai;Nanjing University of Aeronautics and Astronautics;Jiangsu Province Key Laboratory of Aerospace Power Systems;Collaborative Innovation Center of Advanced Aero-Engine;

..............page:640-645

Unsteady Numerical Simulation on Blade Temperature Field of Multi-Stage Axial Turbine
LI Yu-jie;LIU Yong-bao;College of Power Engineering;Naval University of Engineering;

..............page:646-652

An Experimental Study of Effects of Inflow Condition to Boundary Layer of an Ultra-High-Lift LPT at Unsteady State
SUN Shuang;LEI Zhi-jun;LU Xin-gen;ZHAO Sheng-feng;ZHU Jun-qiang;College of Aeronautical Engineering;Civil Aviation University of China;Institute of Engineering Thermophysics;Chinese Academy of Sciences;

..............page:653-661

Research on Thermal Throat of RBCC Based on Heat Distribution
WANG Ya-jun;LI Jiang;HE Guo-qiang;QIN Fei;TANG Xiang;School of Astronautics;Northwestern Polytechnical University;

..............page:662-668

Characteristics of Thermoacoustic Oscillations in MagnesiumBased Water Ramjet
YANG Ya-jing;LI Xiao-ya;JING Hong-da;School of Aerospace;State Key Laboratory for Strength and Vibration of Mechanical Structures;Xi’an Jiaotong University;

..............page:669-674

Emission Characteristics of a Rich-Quench-Lean Trapped-Vortex Combustor Utilizing Quenching Device of Orifice Plate Combined with Bluff-Body
JIANG Bo;HE Xiao-min;JIN Yi;WU Ze-jun;DING Guo-yu;SONG Yao-yu;Nanjing University of Aeronautics and Astronautics;Jiangsu Province Key Laboratory of Aerospace Power Systems;

..............page:675-683

Comparison of Supersonic Combustion Characteristics of Vaporized Kerosene and Ethylene
ZHONG Zhan;WANG Zhen-guo;SUN Ming-bo;Science and Technology on Scramjet Laboratory;National University of Defense Technology;

..............page:684-690

Experimental Investigation on Emission of Lean Premixed Preevaporation Combustor
DENG Yuan-hao;MA Cun-xiang;GUO Kai;XU Hua-sheng;ZHANG Jing-zhou;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Gas Turbine Establishment;

..............page:691-697

Experimental Investigations on Combustion Characteristics of a Vaporized-Flameholder Pilot Combustor in TBCC Engine
ZHU Zhi-xin;HE Xiao-min;Song Yao-yu;ZHU Yi-xiao;QIN Wei-lin;Nanjing University of Aeronautics and Astronautics;Jiangsu Province Key Laboratory of Aerospace Power Systems;Science and Technology on Scramjet Laboratory;Beijing Power Machinery Institute;

..............page:698-705

Large Eddy Simulation of Droplet Breakup in Supersonic Flow
LIU Nan;WANG Zhen-guo;XIAO Feng;SUN Ming-bo;SHEN Zheng;Science and Technology on Scramjet Laboratory;National University of Defense Technology;The 92853 Ttroops of PLA;

..............page:706-712

Quasi-Direct Numerical Simulation on Atomization Characteristics of Impinging Jets Injector
LI Jia-nan;FEI Jun;YANG Wei-dong;ZHOU Li-xin;LIU Chang-bo;Science and Technology on Liquid Rocket Engine Laboratory;

..............page:713-725

Preliminary Experimental Investigation of Solid Fuel Scramjet Combustor
LI Biao;CHI Hong-wei;WANG Li-he;WEI Zhi-jun;WANG Ning-fei;School of Aerospace Engineering;Beijing Institute of Technology;

..............page:726-732

Theoretical and Experimental Investigation on Dynamic Response of Blade with Squeeze-Film Air Damper
CHEN Lu-lu;HONG Jie;MA Yan-hong;AVIC Commercial Aricraft Engine CO.;LTD.;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:733-740

Nonlinear Filter with Inequality Constraints for Turbojet Engine Health Estimation
CHEN Yu;JU Hong-fei;LU Feng;HUANG Jin-quan;Nanjing University of Aeronautics and Astronautics;Jiangsu Province Key Laboratory of Aerospace Power System;Guizhou Liyang Aero-Engine Corporation;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Collaborative Innovation Center of Advanced Aero-Engine;

..............page:741-748

A Comparison Study of Turbo-Shaft Engine Fast Response Control Schemes in Power Recovery Process During Helicopter Autorotation
HUA Wei;DENG Yu;ZHANG Hai-bo;HUANG Jin-quan;Nanjing University of Aeronautics and Astronautics;Jiangsu Province Key Laboratory of Aerospace Power System;China Aviation Industry Corp Aviation Power Control System Research Institute;China Southern Aviation Industry Co.;Ltd.;

..............page:749-757

Numerical Research on Flow Passage of Ram-Rotor Test System
HAN Ji-ang;GUAN Jian;ZHONG Jing-jun;YUAN Chen-guang;Marine Engineering College;Dalian Maritime University;

..............page:758-768

Measurement and Regression-Rate Modification of MA/HTPB/Paraffin Fuels
YAN Wan-hong;ZHANG Wei;ZHOU Xing;LI Ren-jie;BAO Tong;GAO Dong-lei;LI Shi-liang;Institute of Aerospace Science and Engineering;National University of Defense Technology;

..............page:769-775

Mechanical Properties and Constitutive Model for HTPB Propellant under Intermediate Strain Rate Compression
WANG Zhe-jun;QIANG Hong-fu;WANG Guang;LIU Xiao-chuan;WU Wen-ming;Power Engineering Department;Xi’an Hi-Tech Institute;Aircraft Strength Research Institute;

..............page:776-782

Flight Test Performance Evaluation of 20cm Ion Thruster
YANG Fu-quan;JIANG Hao-cheng;ZHANG Tian-ping;GU Zuo;GUO Ning;WANG Xiao-yong;CHEN Xue-kang;Science and Technology on Vacuum & Cryogenics Technology and Physics Laboratory;Lanzhou Institute of Physics;

..............page:783-787

Preliminary Study for Effects of Laser Pulse Width on Propulsion Performance of GAP Propellant Doped with Carbon
WANG Xiao-yong;WU Li-zhi;GUO Ning;HE Nian-bai;SHEN Rui-qi;YE Ying-hua;School of Chemical Engineering;Nanjing University of Science and Technology;Shanghai Space Propulsion Technology Research Institute;

..............page:788-792

Experimental Study of Thermal Characteristics and Thermal Vacuum of LHT-100 Self-Excited Hall Thruster
TIAN Li-cheng;GAO Jun;LI Xing-kun;GUO Ning;GU Zuo;ZHANG Tian-ping;Science and Technology on Vacuum Technology and Physics Laboratory;Lanzhou Institute of Physics;

..............page:793-800