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Journal of Aerospace Power
1000-8055
2015 Issue 7
Velocity and temperature similarity solutions of wedge flow laminar boundary layer with wall injection
ZHAO Guo-chang;DU Xia;SONG Li-ping;SHAN Long;KONG Jing-ru;PENG Da-wei;Faculty of Aerospace Engineering;Shenyang Aerospace University;Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System;Faculty of Aerospace Engineering;Shenyang Aerospace University;Association of Science and Technology;Shenyang Aerospace University;
..............page:1537-1545
Characteristics of low swirl flow and combustion in a limited space
DENG Yang-bo;SONG De-yan;XU Zhen;JIANG Xi;Marine Engineering College;Dalian Maritime University;
..............page:1546-1553
Influences of pressure ratio and Reynolds number on flow characteristics of labyrinth seal in compressor stator well
LIU Gao-wen;CHEN Kai;GANG Tie;ZHENG Hai-liang;School of Power and Energy;Northwestern Polytechnical University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1554-1560
Effects of inlet flow parameters oscillation on combustion instability of gas turbine combustor
XIE Fa;ZHANG Shan-shan;JIANG Hong-de;Gas Turbine Institute;Department of Thermal Engineering;Tsinghua University;Beijing Huatsing Gas Turbine and Integrated Gasification Combined Cycle Technology Company Limited;
..............page:1561-1565
Unsteady swirling flow in low emissions stirred swirls combustor
QIN Hao;DING Zhi-lei;LI Hai-tao;LIN Yu-zhen;LI Ji-bao;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics of Astronautics;Commercial Aircraft Engine Company Limited;Aviation Industry Corporation of China;
..............page:1566-1575
Three-dimensional numerical simulation of the parametric properties of continuously rotating detonation engine
WU Dan;LIU Yan;WANG Jian-ping;Center for Combustion and Propulsion and Center for Application Physics Technology;College of Engineering;Peking University;State Key Laboratory of Turbulence and Complex System;College of Engineering;Peking University;
..............page:1576-1582
Numerical study of flow characteristics in rotating S-shaped passage with ribs
WANG Shun-bin;ZHANG Li;ZHAO Shu;ZHU Hui-ren;SUN Rui-jia;School of Power and Energy;Northwestern Polytechnical University;Turbine Department;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;
..............page:1583-1591
Scrubbing inerting engineering calculations in multi-bay fuel tank of an aircraft
LIU Yu-lin;WANG Xue-de;MU Xiao-hong;YANG Guo-liang;School of Energy and Power Engineering;Nanjing University of Science and Technology;
..............page:1592-1598
Aeroacoustic characteristic of siren incentive system
DING Zhi-lei;LIN Yu-zhen;QIN Hao;TANG Guan-qiong;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics of Astronautics;
..............page:1599-1604
Influence of spray orientation parameters on spray lubrication process of aero spur gears
WANG Yan-zhong;NIU Wen-tao;TANG Wen;GUO Mei;LI Guo-quan;School of Mechanical Engineering and Automation;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1605-1610
Design method and revising strategy of inherent characteristics for dynamical similarity test model of blade
LUO Zhong;GUO Jian;ZHU Yun-peng;WANG De-you;School of Mechanical Engineering and Automation;Northeastern University;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1611-1617
Finite element analysis for the effect of notched radius on fatigue life
JIN Dan;TIAN Da-jiang;LI Jiang-hua;LIN Wei;CHEN Xu;School of Chemical Engineering and Technology;Tianjin University;School of Energy and Power Engineering;Shenyang University of Chemical Technology;
..............page:1618-1623
Influence of contact characteristics on thermal induced vibration of non-continuous rotor
XU Ning;LIU Zhan-sheng;DONG Yan-yang;WANG Zhen-lin;WANG Qing-chao;School of Energy Science and Engineering;Harbin Institute of Technology;Harbin No.703 Research Institute;China Shipbuilding Industry Corporation;
..............page:1624-1631
Comparison of two reliability models for performance degradation analysis
WANG Zhi-hua;ZANG Guang-kui;ZHANG Yong-bo;FU Hui-min;Research Center of Small Sample Technology;Beijing University of Aeronautics and Astronautics;
..............page:1632-1637
Pultrusion and properties of the twisted carbon fiber/phenolic resin Z-pin
ZHANG Xiang-yang;LI Yong;CHU Qi-yi;LI Wen;College of Material Science and Technology;Nanjing University of Aeronautics and Astronautics;
..............page:1638-1644
Experiment of jet noise reduction technology using lobed mixer
SHAO Wan-ren;HE Jing-yu;WU Fei;LI Xiao-dong;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1645-1650
Comparison on aerodynamic and stealthy performance of flying wing unmanned aerial vehicle with three conformal intake inlets
ZHANG Le;ZHOU Zhou;XU Xiao-ping;WANG Hong-bo;State Key Laboratory of UAV Special Technology;Northwestern Polytechnical University;
..............page:1651-1660
Flow field of cylindrical membrane inflation under the fluid-structure interaction
WANG Cong-lei;SUN Jian-hong;XU Chang-yue;HOU Bin;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1661-1669
Transition prediction based on amplification factor and Spalart-Allmaras turbulence model
SHI Ya-yun;BAI Jun-qiang;HUA Jun;YANG Ti-hao;School of Aeronautics;Northwestern Polytechnical University;Chinese Aeronautical Establishment;Aviation Industry Corporation of China;
..............page:1670-1677
Study of variable geometry supersonic inlet aerodynamic performance in a wide Mach number range
ZHAO Hao;XIE Lü-rong;GUO Rong-wei;WANG Jian-yong;ZHANG Jun;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1678-1684
Scramjet nozzle with adjustable cowl scheme
PANG Li-na;XU Jing-lei;GE Jian-hui;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1685-1690
New approach to improve the endwall flow of compressor—leading edge strake blade technique
YI Wei-lin;TANG Fang-ming;CHEN Zhi-min;JI Lu-cheng;School of Mechanical Engineering;Beijing Institute of Technology;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:1691-1698
Aerodynamic optimization for twisted S1 stream surface of multi-stage turbine considering cooling air
WANG Long-fei;WANG Song-tao;LUO Lei;LU Shao-peng;WEN Feng-bo;Engine Aerodynamic Research Center;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:1699-1710
Prediction method of vehicle alternator cooling fan rotation noise
WANG Yuan-wen;DONG Da-wei;YAN Bing;School of Mechanical Engineering;Southwest Jiaotong University;
..............page:1711-1720
Stabilizing analysis of trapezoidal circumferential grooves on an axial rotor
DENG Jing-liang;CHU Wu-li;ZHANG Hao-guang;School of Power and Energy;Northwestern Polytechnical University;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1721-1730
Pumping speed of cryopump for xenon
LING Gui-long;WEI Li-jun;CAI Guo-biao;School of Astronautics;Beijing University of Aeronautics and Astronautics;Unit 93469;the Chinese People’s Liberation Army;
..............page:1731-1736
Abnormal phenomenon of thrust reduction of range rocket nozzle under high altitude condition
ZHANG Fu;WANG Peng-xin;RUAN Wen-jun;WANG Hao;ZHU Chen-guang;School of Energy and Power Engineering;Nanjing University of Science and Technology;Baicheng Ordnance Test Center;the Chinese People’s Liberation Army;School of Chemical Engineering;Nanjing University of Science and Technology;
..............page:1737-1744
Numerical study on the plumes of solid rocket motor under various flight conditions
NIU Qing-lin;FU De-bin;LI Xia;School of Aerospace Engineering;Beijing Institute of Technology;
..............page:1745-1751
Experiment on breakup mechanism of impinging jet of power-law liquid
LI Jian-jun;XIA Zhen-yan;TIAN Yan;School of Mechanical Engineering;Tianjin University;
..............page:1752-1758
Aero-engine condition monitoring method based on cluster features weighting
ZHOU Yuan;ZUO Hong-fu;WANG Li-na;College of Civil Aviation;Nanjing University of Aeronautics and Astronautics;School of Electronic and Information Engineering;Nanjing University of Information Science and Technology;
..............page:1759-1765
Limit management of aircraft engine based on nonlinear model predictive control method
DU Xian;GUO Ying-qing;CHEN Xiao-lei;School of Power and Energy;Northwestern Polytechnical University;
..............page:1766-1771
Design and experiment of hydraulic amplified direct drive valve based on giant magnetostrictive material
YANG Zhao-shu;HE Zhong-bo;YU Jun-tao;LI Dong-wei;Vehicle and Electrical Engineering Department;Ordnance Engineering College;School of Mechanical;Electrical and Information Engineering;Shangdong University;Weihai;
..............page:1772-1783
Engine reverser thrust system safety design
ZHANG Yan-hui;QIN Hao;WANG Dai-jun;Aircraft Propulsion and Fuel System Design and Research Department;the First Aircraft Institute;Aviation Industry Corporation of China;
..............page:1784-1792