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Journal of Propulsion Technology
1001-4055
2015 Issue 5
Thrust Measurement of H2/Air Continuously Rotating Detonation Engine(Ⅱ)- Thrust Under Dual Wave Mode
LIN Wei;ZHOU Jin;LIN Zhi-yong;LIU Shi-jie;Science and Technology on Scramjet Laboratory;National University of Defense Technology;
..............page:641-649
Concentration Measurement of Carbon Monoxide in Combustion Chamber of an ADN-Based Propellant Thruster
ZHANG Wei;SHEN Yan;YU Xi-long;YAO Zhao-pu;WANG Meng;ZENG Hui;LI Fei;ZHANG Shao-hua;Beijing Institute of Control Engineering;China Academy of Space Technology;Key Laboratory of High Temperature Gas Dynamics;Institute of Mechanics;CAS;
..............page:650-655
Three Bearing Swivel Nozzle Vector Deflection Law Study and Fluid Field Calculation
LIU Shuai;WANG Zhan-xue;ZHOU Li;LIU Zeng-wen;School of Power and Energy;Northwestern Polytechnical University;
..............page:656-663
Numerical Simulation of Denotation Wave Induced by Supersonic Projectile using Gridless Method
WU Wei;XU Hou-qian;WANG Liang;XUE Rui;CAI Feng-feng;School of Power Engineering;Nanjing University of Science & Technology;
..............page:664-670
Experimental Investigation on Oblique Shock and Bow Shock Interaction with Rainbow Schlieren
WU Wen-tang;HONG Yan-ji;WANG Dian-kai;LI Qian;YE Ji-fei;JIANG Guan-lei;State Key Laboratory of Laser Propulsion and Application;Academy of Equipment;School of Aerospace;Tsinghua University;Beijing Institute of Tracking and Communication;
..............page:671-677
Effects of Downward-Outward Penetration Angle of an Asymmetric Lobed Mixer on Aero-Thermal Dynamical Performance of an S-Shaped Nozzle
LIU You-hong;DU Li-wei;LI Teng;SHAO Wan-ren;XU Su;DENG Hong-wei;National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics;School of Energy and Power Engineering;Beihang University;Shenyang Aero-Engine Design Institute;Aviation Industry Corporation of China;
..............page:678-687
A Study of Applications of 3D Viscous Inverse Method Based on Transpiration Boundary Conditions for Turbomachinery Aerodynamic Design
YANG Jin-guang;LIU Zhen-de;SHAO Fu-yong;WU Hu;Beijing Power Machinery Institute;State Key Laboratory of Laser Propulsion and Application;Beijing Power Machinery Institute;School of Power and Energy;Northwestern Polytechnical University;
..............page:688-695
Optimization Research on a Novel Turbine Blade Tip Seal Configuration Based on Aerodynamic Performance
LI Yu-jie;LIU Yong-bao;HE Xing;College of Power Engineering;Naval University of Engineering;
..............page:696-702
Experimental Investigation of Airfoil Trailing-Edge Noise Reduction in a Normal Indoor Test Bed
JI Liang;QIAO Wei-yang;WANG Liang-feng;YING Ji-yong;School of Power and Energy;Northwestern Polytechnical University;AVIC Commercial Aircraft Engine Co.;LTD.;
..............page:703-712
Effects of Rotor-Stator Interaction on Flow Field of a Transonic Boundary Layer Suction Compressor
DU Kun;WANG Song-tao;Energy Science and Engineering College;Harbin Institute of Technology;
..............page:713-721
Experimental Investigation on Stall Characteristics on Rotor Tip End-Wall
MA Cai-dong;LI Ying-hong;WU Yun;ZONG Hao-hua;ZHANG Zhi-bo;Science and Technology on Plasma Dynamics Laboratory;Air Force Engineering University;
..............page:722-728
Full Annulus Numerical Simulation of Aerodynamic Stability of Compressor with Total Pressure Distortion
CHEN Jing-hua;TU Bao-feng;Laboratory of Science and Technology on Aero Electromechanical System;Nanjing Engineering Institute of Aircraft Systems;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:729-736
Reaction Kinetic Simulation of Combustion Process in Large Scale Duty Gas Turbine
ZENG Wen;ZHANG Jing-pu;CHEN Bao-dong;MA Hong-an;LIANG Shuang;School of Aerospace Engineering;Shenyang Aerospace University;
..............page:737-744
Design and Output Characteristic of Siren Incentive System
DING Zhi-lei;LIN Yu-zhen;QIN Hao;TANG Guan-qiong;LI Hai-tao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Jet Propulsion;Beijing University of Aeronautics and Astronautics;
..............page:745-751
Effects of Intermediate Reaction Involving HO2 on Simulation of Rocket Plume Afterburning
DUAN Ran;Eriqitai;ZHU Xi-juan;College of Energy and Power Engineering;Beihang University;Science and Technology on Optical Radiation Laboratory;
..............page:752-760
Factors on Affecting Ignition Start-up of Gas Generator with LowBurning Velocity Fuel Rich Propellant
HUANG Hai-long;ZHENG Ri-heng;HU Xiao-bing;LAI Mou-rong;LIU Na;GAO Xin-feng;Beijing Power Machinery Institute;Science and Technology on Scramjet Laboratory;Beijing Power Machinery Institute;
..............page:761-767
Investigation on Dynamical Modeling and Vibration Characteristics for Aero Engine
ZHANG Da-yi;LIU Ye-hui;HONG Jie;MA Yan-hong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:768-773
High Temperature MHD Technology System Design and Commissioning Experiments
GAO Ling;LI Yi-wen;ZHANG Bai-ling;YANG Peng-yu;FAN Hao;DUAN Cheng-duo;XIANG Bo-luo;Plasma-Dynamic Laboratory;Air Force Engineering University;The 95903th Unit of PLA;
..............page:774-779
Flame Stabilization Characteristics of n-Decane and RP3in a Scramjet Combustor
WU Xian;LIN Yu-zhen;LIU Wei;WANG Jian-chen;National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics/School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:780-788
Thermal Hazard Study of Composite Modified Double-Base Propellant with High Solid Content
JIA Hao-nan;LU Gui-e;AN Zhen-tao;JIANG Jin-yong;GE Qiang;WANG Shao-guang;CHEN Chen;Ordnance Engineering College;Ordnance Technology Research Institute;Ordnance Engineering College;
..............page:789-794
Effects of Focusing and Diverging Magnetic Field Topology on Hall Thruster Channel Wall Erosion
DING Yong-jie;HU Yan-lin;YAN Shi-lin;LI Hong;LI Yu-quan;CAI Ning-bo;Advanced Power Technology Institute;Harbin Institute of Technology;Beijing Institute of Control Engineering;
..............page:795-800