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Journal of Aerospace Power
1000-8055
2016 Issue 6
Development trend and characteristics of liquefied natural gas as the aviation fuel
LIU Ai-guo;CHEN Xin;CHEN Bao-dong;ZENG Wen;WANG Cheng-jun;Faculty of Aerospace Engineering;Shenyang Aerospace University;
..............page:1281-1288
Pressure effect on the heat transfer characteristics of hydrocarbon fuel in the horizontal circular tube at supercritical pressures
ZHU Kun;XU Guo-qiang;JIA Zhou-xia;ZHANG Qi-jun;Academy of Aeronautic Propulsion Technology;Aviation Industry Corporation of China;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:1289-1296
Experiment on geometrical limits of gaseous detonation of ethylene/oxygen mixtures in narrow gaps
PAN Zhen-hua;ZHANG Peng-gang;ZHU Yue-jin;PAN Jian-feng;School of Energy and Power Engineering;Jiangsu University;
..............page:1297-1302
Analysis of leakage flow through finger seal based on porous medium
BAI Hua-lei;WANG wei;ZHANG Zhen-sheng;HU Guang-yang;Shenyang Engine Design and Research Institute;Aviation Industry Corporation of China;
..............page:1303-1308
Heat release model related to flame variation mechanism and modal analysis
WANG Kun;FANG Ai-bing;XING Shuang-xi;CUI Yu-feng;NIE Chao-qun;Institute of Engineering Thermophysics;Chinese Academy of Sciences;School of Physical Sciences;University of Chinese Academy of Sciences;
..............page:1309-1317
Numerical simulation of two-phase flow and heat transfer in complex rotating multi-cavity system
LUO Lei;JI Hong-hu;SHI Xiao-juan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1318-1326
Flow and heat transfer characteristics for inter-layer liquid cooling of 3D-IC with staggered micro-pin fins
MA Dan-dan;XIA Guo-dong;ZHAI Yu-ling;LI Yun-fei;JIANG Jing;Key Laboratory of Enhanced Heat Transfer and Energy Conservation;Ministry of Education;School of Environmental and Energy Engineering;Beijing University of Technology;
..............page:1327-1334
Numerical simulation on film cooling characteristics of heart shaped hole
XIAO Yang;JIN Tao;HE Li-ming;DING Wei;L Zhi-hui;DAI Sheng-ji;Aeronautic and Astronautic Engineering College;Air Force Engineering University;Research Institute of Army Aviation;the Chinese People’s Liberation Army;Department of Training;Air Force Engineering University;The 93066Unit;the Chinese People’s Liberation Army;
..............page:1335-1342
Influence of low temperature plasma discharge zone length on ignition initiating
GUO Xiao-jing;ZHENG Dian-feng;YU Yong;ZHANG Hui-qiang;College of Engineering;Peking University;School of Aerospace Engineering;Beijing Institute of Technology;School of Aerospace Engineering;Tsinghua University;
..............page:1343-1350
Effects of incoming boundary layer on injection characteristics of a scramjet combustor
ZHOU Xun-huang;CHEN Rong-qian;YOU Yan-cheng;ZHU Cheng-xiang;HUANG Yue;School of Aerospace Engineering;Xiamen University;
..............page:1351-1358
High temperature fatigue life model for single crystal nickel superalloy based on principal component analysis
WANG Rong-qiao;JIANG Kang-he;HU Dian-yin;JING Fu-lei;SHEN Xiu-li;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Beijing Key Laboratory of Aero-Engine Structure and Strength;Beijing University of Aeronautics and Astronautics;Academy of Aeronautic Propulsion Technology;Aviation Industry Corporation of China;
..............page:1359-1367
Excitation characteristics of rotor/stator-interaction flow field and resonant design of bladed disk
LI Lin;MA Hao-ran;WANG Pei-yi;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1368-1376
Analysis on torsional feature of continuous fiber reinforced metal matrix composite turbine shaft
SHA Yun-dong;JIA Que-yue;LUO Li;ZHAO Feng-tong;LUAN Xiao-chi;Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System;Faculty of Aerospace Engineering;Shenyang Aerospace University;
..............page:1377-1384
Reliability analysis of hierarchical systems based on Bayesian network
LIU Yu;HAN Feng;YAN Kai;LU Xi-cheng;Department of No.5;Northwest Institute of Nuclear Technology;Science and Technology on High Power Microwave Laboratory;Northwest Institute of Nuclear Technology;
..............page:1385-1392
Investigation on disk containment of aero-engine turbine casing
TANG Jin;TANG Guang;XUAN Hai-jun;JIANG You-wei;Aviation Key Laboratory of Aero-engine Vibration Technology;China Aviation Powerplant Research Institute;Aviation Industry Corporation of China;High-Speed Rotating Machinery Laboratory;Institute of Chemical Machinery;Zhejiang University;
..............page:1393-1399
Predominant factor related to stress intensity factor range on creep-fatigue crack growth of nickel-superalloy FGH97
LIU Hao;BAO Rui;YUE Chen-yang;FEI Bin-jun;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1400-1407
A parallel magnetic low stiffness vibration isolator
DONG Guang-xu;ZHANG Xi-nong;LUO Ya-jun;YAN Bo;State Key Laboratory for Strength and Vibration of Mechanical Structures;School of Aerospace;Xi’an Jiaotong University;
..............page:1408-1416
Calculation method of stress intensity factor based on the three-dimensional stress field at the crack tip
JIA Xu;HU Xu-teng;SONG Ying-dong;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;
..............page:1417-1426
Effect of axial spacing between rotor-stator on vibration stress of blade
WANG Xiang-peng;WANG Yan-rong;TIAN Ai-mei;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;Collaborative Innovation Center for Advanced Aero-Engine;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:1427-1434
Aero-engine distributed control system topology optimization method
SONG Jun-qiang;TANG Li-li;PAN Mu-xuan;HUANG Jin-quan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1435-1440
Performance optimization of aeroengine based on Fibonacci search method
YANG Dan-dan;China Gas Turbine Establishment;Aviation Industry Corporation of China;
..............page:1441-1449
Real-time monitor and diagnosis of combustion system based on kernel principal component analysis
ZHU Fei-xiang;LI Ben-wei;ZHAO Yong;SONG Han-qiang;Graduate Students’ Brigade;Naval Aeronautical and Astronautical University;Department of Aircraft Engineering;Naval Aeronautical and Astronautical University;
..............page:1450-1459
Self-scheduled control method for aero-engine based on sum of squares programming of polynomial
WU Bin;HUANG Jin-quan;Jiangsu Province Key Laboratory of Aerospace Power System;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Aviation Motor Control System Institute;Aviation Industry Corporation of China;Collaborative Innovation Center for Advanced Aero-Engine;
..............page:1460-1468
Flow field characteristics of the U-shaped throttling constant differential pressure valve
LI Jia;LI Hua-cong;FU Jiang-feng;WANG Shu-hong;School of Power and Energy;Northwestern Polytechnical University;Xi’an Aero-engine Controls Technology Company Limited;Aviation Industry Corporation of China;
..............page:1469-1476
Effect on parafoil aerodynamic performance of leading edge
NIE Shuai;CAO Yi-hua;TIAN Si-ying;School of Astronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;Aerodynamic Technology Academy;China Aerospace Science and Industry Corporation;
..............page:1477-1485
Synthetical optimization design of rotor airfoil by genetic algorithm
WANG Qing;ZHAO Qi-jun;National key Laboratory of Science and Technology on Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:1486-1495
Vibratory loads prediction of rotor with trailing edge flaps
LIU Shi-ming;YANG Wei-dong;YU Zhi-hao;WU Jie;National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;School of Naval Architecture and Ocean Engineering;Jiangsu University of Science and Technology;
..............page:1496-1503
Flow field simulation and fuel regression rate analysis of HTPB solid fuel ramjet
LI Xin-tian;LU Xin;LI Yan-cheng;LIU Jun-yi;GAO Jing-jing;China Academy of Launch Vehicle Technology;China Aerospace Science and Technology Corporation;
..............page:1504-1510
Design and numerical simulation of oxygen-hydrogen axisymmetric heater with multi-injector
LI Xuan;XU Xu;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:1511-1520
Static characteristics analysis of foil thrust bearing considering the rarefield gas effect
YAN Jia-jia;LIU Zhan-sheng;ZHANG Guang-hui;WEI Ji-qin;School of Energy Science and Engineering;Harbin Institute of Technology;
..............page:1521-1529
A viscous inverse problem method for turbomachinery three-dimensional blade profile
NING Fang-fei;JIA Xin-liang;JU Peng-fei;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamic;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:1530-1536