1005-1120
2013 Issue 2
SIMULATION OF TEMPERATURE FIELD IN ULTRA-HIGH FREQUENCY INDUCTION HEATING AND VERIFICATION
Li Qilin;Xu Jiuhua;Su Honghua;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
Li Qilin;Xu Jiuhua;Su Honghua;College of Mechanical and Electrical Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:155-161
..............page:221
IMPROVED DOPPLER WARPING METHOD FOR AIRBORNE RADAR WITH NON-SIDELOOKING ARRAY
Zhao Jun;Shen Mingwei;Zhu Daiyin;Zhu Zhaoda;Aeronautic Ordnance Engineer Department;The First Aeronautical Institute of Air Force;College of Electronic and Information Engineering;Nanjing University of Aeronautics and Astronautics;College of Computer &Information;Hohai University;
Zhao Jun;Shen Mingwei;Zhu Daiyin;Zhu Zhaoda;Aeronautic Ordnance Engineer Department;The First Aeronautical Institute of Air Force;College of Electronic and Information Engineering;Nanjing University of Aeronautics and Astronautics;College of Computer &Information;Hohai University;
..............page:169-174
DISCONTINUOUS GALERKIN TIME DOMAIN METHOD FOR SOI THIN-RIDGE WAVEGUIDE PROBLEM
Gao Siping;Cao Qunsheng;College of Electronic and Information Engineering;Nanjing University of Aeronautics and Astronautics;
Gao Siping;Cao Qunsheng;College of Electronic and Information Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:162-168
HYBRID AIRFOIL DESIGN FOR FULL-SCALE ICE ACCRETION TEST
Guo Tao;Zhu Chengxiang;Zhu Chunling;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Key Laboratory of Fundamental Science for National Defense Advanced Design Technology of Flight Vehicle;Nanjing University of Aeronautics and Astronautics;
Guo Tao;Zhu Chengxiang;Zhu Chunling;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Key Laboratory of Fundamental Science for National Defense Advanced Design Technology of Flight Vehicle;Nanjing University of Aeronautics and Astronautics;
..............page:139-144
SMOOTHNESS INDICATOR OF WENO SCHEME FOR RESOLVING SHORT WAVE
Wu Conghai;Zhao Ning;Xu Shuang;Wang Donghong;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;College of Science;Nanjing University of Aeronautics and Astronautics;
Wu Conghai;Zhao Ning;Xu Shuang;Wang Donghong;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;College of Science;Nanjing University of Aeronautics and Astronautics;
..............page:125-131
PARAMETRIC MODELING OF COMPONENT LIBRARY FOR LANDING GEAR BASED ON CATIA/CAA
Ren Jie;Nie Hong;Wei Xiaohui;Fu Yongfeng;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
Ren Jie;Nie Hong;Wei Xiaohui;Fu Yongfeng;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:118-124
STRAIGHTFORWARD MULTI-SCALE BOUNDARY ELEMENT METHOD FOR GLOBAL/LOCAL MECHANICAL ANALYSIS OF ELASTIC HETEROGENEOUS MATERIAL
GaoXiguang;Song Yingdong;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;
GaoXiguang;Song Yingdong;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:145-154
CALCULATION FOR KERNEL OF INTERVAL GREY NUMBER BASED ON BARYCENTER APPROACH
Zeng Bo;Liu Sifeng;Chongqing Key Laboratory of Electronic Commerce and Supply Chain System;Chongqing Technology and Business University;Strategical Planning College;Chongqing Technology and Business University;College of Economic and Management;Nanjing University of Aeronautics and Astronautics;
Zeng Bo;Liu Sifeng;Chongqing Key Laboratory of Electronic Commerce and Supply Chain System;Chongqing Technology and Business University;Strategical Planning College;Chongqing Technology and Business University;College of Economic and Management;Nanjing University of Aeronautics and Astronautics;
..............page:216-220
MINIMUM ATTRIBUTE CO-REDUCTION ALGORITHM BASED ON MULTILEVEL EVOLUTIONARY TREE WITH SELF-ADAPTIVE SUBPOPULATIONS
Ding Weiping;Wang Jiandong;College of Computer Science and Technology;Nanjing University of Aeronautics and Astronautics;State Key Laboratory for Novel Software Technology;Nanjing University;
Ding Weiping;Wang Jiandong;College of Computer Science and Technology;Nanjing University of Aeronautics and Astronautics;State Key Laboratory for Novel Software Technology;Nanjing University;
..............page:175-184
MULTI-OBJECTIVE PROGRAMMING FOR AIRPORT GATE REASSIGNMENT
Li Junhui;Chen Xin;Zhu Jinfu;College of Economics and Management;Nanjing University of Aeronautics and Astronautics;Guangdong Airport Management Company;Traffic College;Southeast University;
Li Junhui;Chen Xin;Zhu Jinfu;College of Economics and Management;Nanjing University of Aeronautics and Astronautics;Guangdong Airport Management Company;Traffic College;Southeast University;
..............page:209-215
ACTIVE VIBRATION CONTROL OF TWO-BEAM STRUCTURES
Chen Tao;Wang Ligang;Feng Guofeng;College of Science;Harbin Engineering University;
Chen Tao;Wang Ligang;Feng Guofeng;College of Science;Harbin Engineering University;
..............page:193-201
FLEXURAL CAPACITY OF RC BEAM STRENGTHENED WITH PRESTRESSED C/AFRP SHEETS
Wang Xiaomeng;Zhou Chuwei;Ai Jun;Zhang Jian;Wang Dong;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;Lianyungang Highway Management Office;
Wang Xiaomeng;Zhou Chuwei;Ai Jun;Zhang Jian;Wang Dong;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;State Key Laboratory of Mechanics and Control of Mechanical Structures;Nanjing University of Aeronautics and Astronautics;Lianyungang Highway Management Office;
..............page:202-208
OUTPUT MAXIMIZATION CONTROL FOR VSCF WIND ENERGY CONVERSION SYSTEM USING EXTREMUM CONTROL STRATEGY
Fu Dafeng;Ma Yundong;College of Automation Engineering;Nanjing University of Aeronautics and Astronautics;
Fu Dafeng;Ma Yundong;College of Automation Engineering;Nanjing University of Aeronautics and Astronautics;
..............page:185-192
SIMULATION OF BLEED AIR BEHAVIOR DURING AIRCRAFT IN FLIGHT BASED ON FLOWMASTER
ShiHong;Jiang Yanlong;Liu Zhili;Kang Na;Yu Lei;Liu Chao;Du Yanping;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Shanghai Aircraft Design & Research Institute;Commercial Aircraft Corporation of China;Ltd;
ShiHong;Jiang Yanlong;Liu Zhili;Kang Na;Yu Lei;Liu Chao;Du Yanping;College of Aerospace Engineering;Nanjing University of Aeronautics and Astronautics;Shanghai Aircraft Design & Research Institute;Commercial Aircraft Corporation of China;Ltd;
..............page:132-138
APPLICATION OF HYBRID GENETIC ALGORITHM IN AEROELASTIC MULTIDISCIPLINARY DESIGN OPTIMIZATION OF LARGE AIRCRAFT
Tang Changhong;Wan Zhiqiang;School of Mechanical and Engineering;Northwestern Polytechnical University;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
Tang Changhong;Wan Zhiqiang;School of Mechanical and Engineering;Northwestern Polytechnical University;School of Aeronautic Science and Engineering;Beijing University of Aeronautics and Astronautics;
..............page:109-117