1000-8055
2013 Issue 11
..............page:2396
Design analysis of active cooling composite combustion chamber with thin wall
ZHANG Jun-feng;MU Dan;BIAN Xiang-de;Key Laboratory for Mechanics in Fluid Solid Coupling Systems Institute of Mechanics;Chinese Academy of Sciences;
ZHANG Jun-feng;MU Dan;BIAN Xiang-de;Key Laboratory for Mechanics in Fluid Solid Coupling Systems Institute of Mechanics;Chinese Academy of Sciences;
..............page:2401-2407
Effects of combustion heating vitiated air on kerosene-fueled scramjet performance
CHEN Liang;SONG Wen-yan;LUO Fei-teng;LIU Hao;LI Jian-ping;School of Power and Energy;Northwestern Polytechnical University;
CHEN Liang;SONG Wen-yan;LUO Fei-teng;LIU Hao;LI Jian-ping;School of Power and Energy;Northwestern Polytechnical University;
..............page:2408-2418
A spongy icing model for aircraft icing and application
LI Xin;BAI Jun-qiang;WANG Kun;School of Aeronautics;Northwestern Polytechnical University;
LI Xin;BAI Jun-qiang;WANG Kun;School of Aeronautics;Northwestern Polytechnical University;
..............page:2419-2429
Numerical simulation and experiment on air-assisted direct injection injector dynamic spray field
CHENG Qiang;ZHANG Zhen-dong;XIE Nai-liu;School of Energy and Power Engineering;University of Shanghai for Science and Technology;
CHENG Qiang;ZHANG Zhen-dong;XIE Nai-liu;School of Energy and Power Engineering;University of Shanghai for Science and Technology;
..............page:2430-2439
Effect of film cooling on flow and heat transfer of flat tip in transonic turbine cascade
ZHOU Kai;ZHOU Chao;ZHONG Fang-pan;College of Engineering;Peking University;
ZHOU Kai;ZHOU Chao;ZHONG Fang-pan;College of Engineering;Peking University;
..............page:2440-2447
Flow field and film cooling characteristics in supersonic turbine cascade
CHEN Si-jie;SHAN Yong;ZHANG Jing-zhou;TAN Xiao-ming;FEI Wei-wei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
CHEN Si-jie;SHAN Yong;ZHANG Jing-zhou;TAN Xiao-ming;FEI Wei-wei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2448-2454
LES of direct detonation induced by incident circular shock wave focusing
BAO Xing-dong;LI Zhi-qiang;TUO Huan;DONG He;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
BAO Xing-dong;LI Zhi-qiang;TUO Huan;DONG He;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:2455-2461
Atomization characteristics of fuel injector and cavity-based strut flame stabilizer under close-range matching condition
LUO Lian-jun;LIU Yu-ying;ZHANG Wen-long;JI He-ming;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
LUO Lian-jun;LIU Yu-ying;ZHANG Wen-long;JI He-ming;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2462-2467
Analysis on flow and infrared radiation characteristics of double S-nozzle
ZHANG Ye-chuan;WANG Zhan-xue;SHI Jing-wei;FANG Li;KONG De-ying;School of Power and Energy;Northwestern Polytechnical University;The First Aircraft Institute Aviation Industry Corporation of China;
ZHANG Ye-chuan;WANG Zhan-xue;SHI Jing-wei;FANG Li;KONG De-ying;School of Power and Energy;Northwestern Polytechnical University;The First Aircraft Institute Aviation Industry Corporation of China;
..............page:2468-2474
Static aeroelastic problems of transonic fan blades
ZHENG Yun;WANG Biao;YANG Hui;Aeroengine Numerical Simulation Research Center;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
ZHENG Yun;WANG Biao;YANG Hui;Aeroengine Numerical Simulation Research Center;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2475-2482
Numerical simulation of inter-stage bleeding in highly-loaded multistage axial compressor
SHA Xin-guo;YAN Ming;LIU Zheng-liang;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;China Academy of Aerospace Aerodynamics;China Aerospace Science and Technology Corporation;
SHA Xin-guo;YAN Ming;LIU Zheng-liang;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;China Academy of Aerospace Aerodynamics;China Aerospace Science and Technology Corporation;
..............page:2483-2494
CFD result validation and analysis of a subsonic centrifugal compressor impeller with splitter blades
LI Pei-yuan;GU Chun-wei;Key laboratory for Thermal Science and Power Engineering of Ministry of Education;Department of Thermal Engineering;Tsinghua University;
LI Pei-yuan;GU Chun-wei;Key laboratory for Thermal Science and Power Engineering of Ministry of Education;Department of Thermal Engineering;Tsinghua University;
..............page:2495-2502
Effect of slotted blade on performance of high-turning angle compressor cascades
WU Pei-gen;WANG Ru-gen;LUO Kai;GUO Fei-fei;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
WU Pei-gen;WANG Ru-gen;LUO Kai;GUO Fei-fei;Aeronautics and Astronautics Engineering College;Air Force Engineering University;
..............page:2503-2509
Measurement of flow field in compressor stator passages
LUO Ju;HU Jun;YAN Wei;ZHANG Chen-kai;YIN Chao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
LUO Ju;HU Jun;YAN Wei;ZHANG Chen-kai;YIN Chao;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2510-2516
Effect of tip clearance leakage on performance of centimetre-level high subsonic micro axial flow turbine
YU Haibin;DENG Yang;XIA Chen;FU Xin;HUANG Guo-ping;Department of Aviation Mechanical Engineering;Qingdao Branch of Naval Aviation Engineering Institute;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
YU Haibin;DENG Yang;XIA Chen;FU Xin;HUANG Guo-ping;Department of Aviation Mechanical Engineering;Qingdao Branch of Naval Aviation Engineering Institute;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2517-2525
Experiment on aerodynamic performance of APU air inlet system with perforated plate
WANG Ming-sheng;WANG Hu-shan;LI Qiang;HUANG Guo-ping;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
WANG Ming-sheng;WANG Hu-shan;LI Qiang;HUANG Guo-ping;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2526-2535
Hybrid LES/RANS simulation of transverse sonic injection in supersonic turbulent boundary layer
CHEN Ti;LIU Wei-dong;SUN Ming-bo;FAN Xiao-qiang;LIANG Jian-han;College of Astronautics and Material Engineering;National University of Defense Technology;
CHEN Ti;LIU Wei-dong;SUN Ming-bo;FAN Xiao-qiang;LIANG Jian-han;College of Astronautics and Material Engineering;National University of Defense Technology;
..............page:2536-2542
Modified axisymmetric basic flowfield for hypersonic inward turning inlet
LI Yong-zhou;ZHANG Kun-yuan;LUO Lei;WANG Lei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
LI Yong-zhou;ZHANG Kun-yuan;LUO Lei;WANG Lei;College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:2543-2552
Effect of asymmetric ground effect on stabilitiy of tailless aircraft
YANG Mu-qing;MA Dong-li;School of Aeronautics Science and Engineering;Beijing University of Aeronautics and Astronautics;
YANG Mu-qing;MA Dong-li;School of Aeronautics Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2553-2560
Performance simulation and verification of air-turbo-ramjet
LI Cheng;ZHOU Zheng;TU Qiu-ye;CAI Yuan-hu;School of Power and Energy;Northwestern Polytechnical University;
LI Cheng;ZHOU Zheng;TU Qiu-ye;CAI Yuan-hu;School of Power and Energy;Northwestern Polytechnical University;
..............page:2561-2566
Optimum design method of acceleration and deceleration control schedule for gas turbine engine
SHI Yang;TU Qiu-ye;CAI Yuan-hu;QIU Chao;TAN Zhi-yong;School of Power and Energy;Northwestern Polytechnical University;Commercial Aircraft Engine Corporation Limited Aviation Industry Corporation of China;
SHI Yang;TU Qiu-ye;CAI Yuan-hu;QIU Chao;TAN Zhi-yong;School of Power and Energy;Northwestern Polytechnical University;Commercial Aircraft Engine Corporation Limited Aviation Industry Corporation of China;
..............page:2567-2571
Numerical simulation of meso-mechanical response for superalloy ZSGH4169
YU Duo-kui;YANG Xiao-guang;ZHANG Ke-shi;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;School of Civil and Architectural Engineering;Guangxi University;
YU Duo-kui;YANG Xiao-guang;ZHANG Ke-shi;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;School of Civil and Architectural Engineering;Guangxi University;
..............page:2572-2578
Dynamic response analysis and wall thickness optimization of detonation combustor under actual detonation loading
ZHENG Long-xi;CHEN Jing-bin;HUANG Xi-qiao;LU Jie;CHEN Xing-gu;School of Power and Energy;Northwest Polytechnical University;
ZHENG Long-xi;CHEN Jing-bin;HUANG Xi-qiao;LU Jie;CHEN Xing-gu;School of Power and Energy;Northwest Polytechnical University;
..............page:2579-2586
Fatigue life prediction model based on critical plane of nickel-based single crystal superalloy
WANG Rong-qiao;JING Fu-lei;HU Dian-yin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
WANG Rong-qiao;JING Fu-lei;HU Dian-yin;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2587-2592
Multi-plane and multi-critical transient dynamic balance method based on rising speed response information of flexible rotor system
YUE Cong;REN Xing-min;DENG Wang-qun;YANG Yong-feng;Institute of Vibration Engineering;School of Mechanics;Civil Engineering and Architecture;Northwestern Polytechnical University;China Aviation Dynamical Machinery Research Institute Aviation Industry Corporation of China;
YUE Cong;REN Xing-min;DENG Wang-qun;YANG Yong-feng;Institute of Vibration Engineering;School of Mechanics;Civil Engineering and Architecture;Northwestern Polytechnical University;China Aviation Dynamical Machinery Research Institute Aviation Industry Corporation of China;
..............page:2593-2599
Fault diagnosis of roller bearings based on chirplet path pursuit and order cyclostationary demodulation
XU Ya-jun;YU De-jie;LIU Jian;State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body;College of Mechanical and Vehicle Engineering;Hunan University;
XU Ya-jun;YU De-jie;LIU Jian;State Key Laboratory of Advanced Design and Manufacturing for Vehicle Body;College of Mechanical and Vehicle Engineering;Hunan University;
..............page:2600-2608
Improved unstructured grid optimization method based on spring analogy
WANG Guang-xing;YUE Ming;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
WANG Guang-xing;YUE Ming;School of Energy and Power Engineering;Beijing University of Aeronautics and Astronautics;
..............page:2609-2614
Numerical investigation of nozzle flow separation control by injecting secondary jet from nozzle exit
LI Bo;WANG Yi-bai;YANG Li-jun;CHENG Cheng;School of Astronautics;Beijing University of Aeronautics and Astronautics;
LI Bo;WANG Yi-bai;YANG Li-jun;CHENG Cheng;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:2615-2620
Two-phase flow numerical calculation of H2O2/HTPB hybrid rocket engine with diaphragm in grain
WANG Peng-fei;TIAN Hui;YU Nan-jia;CAI Guo-biao;School of Astronautics;Beijing University of Aeronautics and Astronautics;
WANG Peng-fei;TIAN Hui;YU Nan-jia;CAI Guo-biao;School of Astronautics;Beijing University of Aeronautics and Astronautics;
..............page:2621-2626
Design of data acquisition system for solid-liquid dynamic sounding rocket
XIN Jie;CAI Guo-biao;SONG Jia;School of Astronautic;Beijing University of Aeronautics and Astronautics;
XIN Jie;CAI Guo-biao;SONG Jia;School of Astronautic;Beijing University of Aeronautics and Astronautics;
..............page:2627-2633
Adaptive global fast non-singular Terminal sliding mode control for aero-engine
MIAO Zhuo-guang;XIE Shou-sheng;ZHANG Bo;REN Li-tong;WANG Li-guo;WU Yong;Aeronautics and Astronautics Engineering College;Air Force Engineering University;The Unit 95961 the Chinese People’s Liberation Amay;The Unit 61769 the Chinese People’s Liberation Army;Army Aviation Research Institute the Headquarters of the General staff;the Chinese People’s Liberation Army;
MIAO Zhuo-guang;XIE Shou-sheng;ZHANG Bo;REN Li-tong;WANG Li-guo;WU Yong;Aeronautics and Astronautics Engineering College;Air Force Engineering University;The Unit 95961 the Chinese People’s Liberation Amay;The Unit 61769 the Chinese People’s Liberation Army;Army Aviation Research Institute the Headquarters of the General staff;the Chinese People’s Liberation Army;
..............page:2634-2640
..............page:2641-2642