Experiment of flow field in lobed mixer
ZHANG Zhe-heng;WANG Dong-ming;ZHANG Bao-hua;HU Wen-cheng;YU Ting-ting;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:1761-1768

NOx emissions of kerosene combustion at elevated pressure jet stirred combustion reactor
ZHANG Chi;TIAN Ye;XUE Xin;LIN Yu-zhen;XU Quan-hong;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:1769-1774

Effects of swirler structure on the performance of lean-direct-injection combustor
ZENG Qing-hua;KONG Wen-jun;AI Yu-hua;WANG Bao-rui;SUI Chun-jie;Key Laboratory of Light-duty Gas-turbine;Institute of Engineering Thermophysics;Chinese Academy of Sciences;University of Chinese Academy of Sciences;

..............page:1775-1781

Experiment on effect of Knudsen number on micro-scale similarity flow characteristics
ZHENG Jie;ZHU Hui-ren;GUO Tao;MENG Tong;WU A-sai;LU Hong-kang;School of Power and Energy;Northwestern Polytechnical University;

..............page:1782-1788

Effect of spirality flow on heat transfer in rotating limited lamilloy
BAI Guo-qiang;CHANG Hai-ping;Jiangsu Province Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1789-1795

Deflagration to detonation transition characteristic in U-bend square tube
WANG Wei;QIU Hua;FAN Wei;XIONG Cha;School of Power and Energy;Northwestern Polytechnical Univercity;

..............page:1796-1801

Numerical simulation on gas-liquid two-phase detonation combustion induced by shock wave focusing
YANG Qing;LI Zhi-qiang;DI Ya-chao;XU Huan;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:1802-1809

Numerical simulation on infrared radiation characteristics of round to rectangular nozzles with different chevrons considering engine components
LI Wei;ZHANG Bo;WANG Fei;JI Hong-hu;HUA Jia;ZHANG Zong-bin;LUO Ming-dong;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Department of Conceptual Design;Chengdu Aircraft Design and Research Insititute;Aviation Industry Corporation of China;

..............page:1810-1816

Experimental technique and its validation for heat transfer in cooling channels at high rotation numbers
CHENG Jun-hua;NI Bin;DENG Hong-wu;TIAN Shu-qing;CHEN Hao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Research and Development Center;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;

..............page:1817-1823

Deviation angle models suitable for wider range of blade profile camber in axial-flow compressor
LIU Bo;MA Nai-xing;YANG Xiao-dong;CAO Zhi-yuan;School of Power and Energy;Northwestern Polytechnical University;

..............page:1824-1831

Algorithm for constructing the line-shape feature point clouds of aero-engine ruled blades
ZHOU Yu;WANG Hao-chen;DU Fa-rong;School of Transportation Science and Engineering;Beijing University of Aeronautics and Astronautics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;

..............page:1832-1837

Prediction method of stall margin in axial-flow transonic compressor
ZHONG Yong-jian;TENG Jin-fang;XU Xi;QIANG Xiao-qing;WU Ya-dong;OUYANG Hua;School of Aeronautics and Astronautics;Shanghai Jiao Tong University;School of Mechanical Engineering;Shanghai Jiao Tong University;

..............page:1838-1845

Flutter analysis of turbomachinery based on phase lagged boundary condition
YANG Xiao-dong;HOU An-ping;LI Man-lu;WANG Rui;ZHOU Sheng;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:1846-1854

Optimization of aspirated airfoil based on artificial bee colony algorithm and NURBS
YANG Xiao-dong;LIU Bo;ZHANG Guo-chen;NA Zhen-zhe;School of Power and Energy;Northwestern Polytechnical University;

..............page:1855-1862

Numerical study on effects of blade tip air jet on the flow field of wind turbine blade tip
GAO Xiang;HU Jun;WANG Zhi-qiang;Jiangsu Province Key Laboratory of Aerospace Power Systems;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Co-Innovation Center for Advanced Aero-Engine;

..............page:1863-1870

Optimization design for aspirated compressor airfoil and aspiration plan
LI Jun;LIU Bo;YANG Xiao-dong;SHI Lei;School of Power and Energy;Northwestern Polytechnical University;

..............page:1871-1877

Overview of several ice accretion effects on aircraft flight dynamics
SU Yuan;XU Zhong-da;WU Zhen-long;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;

..............page:1878-1893

Strongly coupled RANS algorithm for simulating hovering rotor flow
JI Chang-rui;YANG Xiao-quan;YANG Ai-ming;SI Jiang-tao;LIU Pei-qing;School of Aeronautical Science and Engineering;Beijing University of Aeronautics and Astronautics;Shanghai Aircraft Design and Research Institute;Commercial Aircraft Corporation of China;Ltd.;Department of Mechanics and Mechanical Engineering Science;Fudan University;

..............page:1894-1903

Applicability investigation about several common schemes and turbulence models in high speed flow
SHI Lei;YAN Ming;YANG Yun-jun;ZHOU Wei-jiang;China Academy of Aerospace Aerodynamics;China Aerospace Science and Technology Corporation;

..............page:1904-1910

Radar cross section characteristics of rotor based on computational electromagnetics method
JIANG Xiang-wen;ZHAO Qi-jun;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1911-1921

Effect of active blade pitch control on helicopter rotor performance
WANG Chao;LU Yang;CHEN Ren-liang;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1922-1929

Adaptive artificial viscosity entropy stable scheme for hyperbolic conservation laws
REN Jiong;FENG Jian-hu;LIANG Nan;LIU You-qiong;School of Sciences;Chang’an University;

..............page:1930-1939

Dynamic analysis of rotor-ball bearings system based on elasto-hydrodynamic lubrication with rubbing-misalignment coupling fault
ZHANG Jun-hong;MA Liang;MA Wen-peng;WANG Jun;BA Lin;LI Shu-ming;State Key Laboratory of Engines;School of Mechanical Engineering;Tianjin University;School of Meterials Science and Engineering;Tianjin University;College of Aeronautical Engineering;Civil Aviation University of China;

..............page:1940-1952

Vibration reduction optimization design for parameterized composite blade
CHEN Kun;LIU Yong;ZHANG Cheng-lin;NI Xian-ping;National Key Laboratory of Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1953-1960

Dynamics and reliability for rubbing rotor considering the characteristic of parameter’s random distribution
YANG Le-chang;ZHANG Jian-guo;SUN Jing;HAN Jian-chao;Science and Technology Laboratory on Reliability and Environmental Engineering;School of Reliability and Systems Engineering;Beijing University of Aeronautics and Astronautics;Beijing Satellite Manufacturer;China Academy of Space Technology;China Aerospace Science and Technology Corporation;

..............page:1961-1967

Method of confirming prior parameters value during complexity equipment system testability evaluation with small sample
ZHANG Xi-shan;HUANG Kao-li;YAN Peng-cheng;LIAN Guang-yao;WANG Shao-guang;Ordnance Engineering College;Ordnance Technological Research Institute;

..............page:1968-1973

Fault processing policy based on dual-redundant control law for aero-engine control sensors
JIANG Cai-hong;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;

..............page:1974-1980

Multi-objective optimization design of slipper film in aero-engine fuel piston pump
XU Pei-pei;YE Zhi-feng;WANG Bin;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;

..............page:1981-1986

Modeling method of bearing chamber oil/air two-phase flow under multi-geometrical conditions
SUN Heng-chao;CHEN Guo-ding;CHEN Bo;School of Mechanical Engineering;Northwestern Polytechnical University;

..............page:1987-1995

Denoising method for electrostatic monitoring signal of roller bearing based on spectrum interpolation and difference spectrum of singular value
ZHANG Ying;ZUO Hong-fu;TONG Pei-sheng;CHEN Zhi-xiong;BAI Fang;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;School of Aircraft Engineering;Nanchang Hangkong University;

..............page:1996-2002

Classification of corner vortex shedding in solid rocket motor
ZHANG Xiang-yu;HE Guo-qiang;LIU Pei-jin;National Key Laboratory of Combustion;Thermal Structure and Flow Field;Northwestern Polytechnical University;Xi’an Aerospace Propulsion Institute;Academy of Aerospace Solid Propulsion Technology;China Aerospace Science and Technology Corporation;

..............page:2003-2011

Notch strength and notch sensitivity of double base propellant
HU Shao-qing;JU Yu-tao;WEI Zhen;ZHOU Chang-sheng;School of Mechanical Engineering;Nanjing University of Science and Technology;

..............page:2012-2016