apisat-2014 - 2014 Asia-Pacific International Symposium on

Transcription

APISAT-2014
2014 Asia-Pacific International
Symposium on Aerospace Technology
program(Draft)
24-26 September
Shanghai China
Hosted by
CSAA
Chinese Society of Aeronautics
and Astronautics
Co-organized by
RAeS
Australian Division of the Royal
Aeronautical Society
KSAS
Korean Society for Aeronautical
and Space Sciences
JSASS
Japan Society for Aeronautical
and Space Sciences
APISAT-2014
program
Contents
Welcome Message from Presdient of CSAA
2
Welcome Message from International ProgramChairman of APISAT 2014
3
About APISAT
4
Organizing Committee
5
Schedule at a Glance
6
Plenary Lectures
7
Invited Lecture
10
Technical Session Program
11
Parallel Session Schedule
14
Registration35
Social Events 37
General Information
40
about shanghai
45
Reception
Banquet and performance
Post tour
Conference Venu13
Transportation
Accommodation14
Currency15
Abstracts
3
APISAT-2014
program
4
Welcome Message from Presdient of CSAA
APISAT-2014
program
Welcome Message from International Program
Chairman of APISAT 2014
5
APISAT-2014
program
About APISAT
Organization
The Asia-Pacific International Symposium on Aerospace Technology (abbreviated title: APISAT) is
co-organized by the following four societies (in alphabetical order):
• Australian Division of the Royal Aeronautical Society (RAeS Australian Division)
• Chinese Society of Aeronautics and Astronautics (CSAA)
• Japan Society for Aeronautical and Space Sciences (JSASS)
• Korean Society for Aeronautical and Space Sciences (KSAS)
Aim and Scope
Asia-Pacific International Symposium on Aerospace Technology (APISAT) is the collaborative
endeavor among the Chinese, Australian, Korean and Japanese societies for aerospace sciences. It
provides the opportunity to Asia-Pacific nations for the researchers of universities and academic
institutes, and for the industry engineers to discuss the current and future advanced topics in
aeronautical and space engineering. The official language of this symposium is English.
Topics
6
Topics include but are not limited to:
Aerodynamics and Design
• Computational Fluid Dynamics
• Wind Tunnel Testing
• Flow Visualization
• Unsteady Aerodynamics
• Acoustics
• Aircraft, Helicopter and UAV Design
Dynamics/Control/Avionics
• Flight Simulation
• Navigation
• Guidance and Control
• ATM/CNS
• Sensors and Actuators
• Satellite Attitude Control
Structures and Materials
• Structural Analysis
• Structural Testing
• Smart Structures
• Composite Structures
• Structural Dynamics
• Aeroelasticity
Combustion and Propulsion
• Combustion Analysis
• Fuel Injection
• Turbines
• Engines
• Cooling Systems
• Spacecraft Propulsion
APISAT-2014
Executive Committee
program
Organization Committee
Gaozhuo Liu (President, CSAA)
Noel Schmidt (President, RAeS Australian Division)
Myung Seong Kim (President, KSAS)
Seiya Ueno (President, JSASS)
International Program Committee
Chairman: Haiyan Hu (CSAA)
Co-Chairman:
Cees Bil (RAeS Australian Division)
In Hee Hwang (KSAS)
Takeshi Tsuchiya (JSASS)
Member:
Song Fu (CSAA)
Xiaolin Liu (RAeS Australian Division)
Jae-Woo Lee(KSAS)
Hitoshi Arizono (JSASS)
National Organizing Committee (CSAA)
Chairman Haiyan Hu
Vice Chairman Song Wu
Member:
Jun Hua, Jun Zhou, Degang Cui, Zhenghong Gao, Weijia Huang, Jinsong Leng, Pinqi Xia,
Juen Zhang, Jinxi Ma, Zhihui Tao, Guoqing Wang, Zhiren Han
Secretariat
Xue Zhang/Ce Yu
National Organizing Committee (RAeS Australian Division)
Chairman: Cees Bil
Member
Xiaolin Liu, Don Love, Hideaki Ogawa, Richard Morgan
National Organizing Committee (KSAS)
Chairman: In Hee Hwang
Vice Chairman: Jae-Woo Lee
Member
Hong-Gye Sung, Jeong-Yeol Choi
Secretariat
Cheolkeun Ha
National Organizing Committee (JSASS)
Chairman: Takeshi Tsuchiya
Member: Suguru Hase, Masahiro Kanazaki, Takuji Kishimoto, Zhong Lei,
Tomoyuki Okita Secretariat: Hitoshi Arizono
7
APISAT-2014
program
Schedule at a Glance
Date: Sep. 23-26,2014
Venue: Pullman Shanghai South Hotel
Date
Sep. 23
Tuesday
Sep. 24
Wednesday
Sep. 25
Thursday
Sep. 26
Friday
Time
Function
14:00-21:00
On-site registration
08:30-08:45
08:45-09:45
09:45-10:45
10:45-11:00
11:00-12:00
12:00-13:00
13:30-18:40
Opening ceremony
Plenary lecture(China)
Plenary lecture(Australia)
Coffee break
Parallel sessions
Buffet
Parallel sessions
19:00-20:00
Reception
08:45-09:45
09:45-10:45
10:45-11:45
11:45-12:00
Plenary lecture(Korea)
Plenary lecture(Japan)
Invited lecture (China)
Coffee break
12:00-13:00
Buffet
13:30-18:55
19:00-20:30
Parallel sessions
Banquet
Technical visit to COMAC
Shanghai Aircraft
Manufacturing Center
(SAMC)
Lunch
Visit Shanghai Museum
Dinner
Cruise on the Huangpu River
Back to the hotel
9:00-11:30
12:00-13:00
14:00-17:00
17:30-18:30
19:00-21:00
21:00
8
Location
Hotel Lobby
Ballroom 1+2 (3rd floor)
Room 1、2、3、5、6、7、8 (3rd floor)
Ballroom 3
Room 1、2、3、5、6、7、8
Ballroom 1+2
Coupon is required.
Ballroom 1+2
Ballroom 3
Coupon is required.
Room 1、2、3、5、6、7、8
Ballroom 1+2
Meet in front of the venue at 9:00.
Depart at 9:10 on time.
Coupon is required.
APISAT-2014
program
Plenary Lecture:September 24 Wednesday 08:45 - 10:45
Lecture 1 China
08:45 - 09:45
Lecture 2 AUSTRALIA
09:45 - 10:45
Development of
High-Performance
Structural
Composites with
Mutltifunctionality
for Aerospace
Application
Xiaosu Yi, Director, Science &
Technology Committee, Beijing
Institute of Aeronautical Materials
(BIAM) of AVIC
AVIC Composites Center (ACC)
Asia-Pacific Air
Transport - The next
20 Years
John Vincent, BE Aero (Hons)
Adjunct Professor at the University
of New South Wales Board Director
of the Qantas Foundation Memorial
Ltd.
Plenary Lecture:September 25 Thursday 08:45 - 10:45
Lecture 3 KOREA
08:45 - 09:45
Lecture 4 JAPAN
09:45 - 10:45
Autonomous MultiUAV System for
Cooperative
Transportation
Min-Jea Tahk, Prof.-Division of
Aerospace Engineering
Korea Advanced Institute of Science
and Technology
Long-Term Vision
of Future Air Traffic
Systems in Japan
Yutaka Fukuda, Deputy DirectorAir Traffic Management Department
Electronic Navigation Research
Institute
9
APISAT-2014
program
CHINA
Lecture Title
Development of High-Performance Structural Composites with
Mutltifunctionality for Aerospace Application
Lecturer
Prof. Xiaosu Yi
Affiliation
Director, Science & Technology Committee, Beijing Institute of Aeronautical Materials (BIAM)
of AVIC
AVIC Composites Center (ACC)
Mr. Xiaosu Yi received his master degree and doctor degree respectively in 1982 and 1986 in Materials
Process Engineering at University of Paderborn, Germany. He became a full professor in Polymer Materials
and Technology at Zhejiang University in 1988 and joined Beijing Institute of Aeronautical Materials (BIAM)
since 1998, where he has been the member of the executive board and the director of the Science & Technology
Committee. He is the Senior Chief Scientist of Aviation Industry of China (AVIC) in composite materials and
technology.
Prof. Yi received SAMPE FELLOW AWARD in 2011 and became the Academician of APAM (Asia-Pacific
Academy of Materials) in 2013. He is also the Chairman of SAMPE Beijing Chapter, the executive council
member of International Conference of Composite Materials (ICCM) and Asia-pacific Conference of Composite
Materials (ACCM), Vice Chairman of Materials Engineering Committee of Chinese Society of Aeronautics and
Astronautics(CSAA), Senior member of the Chinese Composites Society, etc. Prof. Yi is also the chief editor of
the Chinese Composite Journal (Acta Materiae Compositae Sinica).
He has published about 400 scientific and technical papers in international and domestic journals. About 60
invention patents were awarded to him. His research interests include structural composites, polymer materials,
functional composites, process engineering, materials modeling and GREEN material technology.
AUSTRALIA
Lecture Title Asia-Pacific Air Transport - the Next 20 Years
Lecturer
Prof. John Vincent
Affiliation
Adjunct Professor at the University of New South Wales
Board Director of the Qantas Foundation Memorial Ltd.
John has extensive airline engineering and maintenance experience over a professional career spanning more than
40 years, including more than 25 years in executive and general management roles in large airline Engineering
and Maintenance organisations.
He is an Aeronautical Engineer, having worked in airline technical services (structures and systems), aircraft
performance, fleet assessment and aircraft acceptance/delivery roles. He has filled senior engineering,
maintenance, fleet development, safety, quality and risk management roles including holding various National
Airworthiness Authority (CASA) approvals and has led the Engineering and Maintenance businesses of Air
Pacific (Fiji), Ansett Australia and Qantas Airways Ltd.
His main career focal areas have been leadership development, business strategy, business process improvement,
change management, governance, regulatory compliance, operational and occupational safety systems, risk
management, employee engagement/communication and relationship management.
He is Adjunct Professor with the University of New South Wales School of Aviation, a Board Director of the
Qantas Foundation Memorial Ltd and President-elect of the Royal Aeronautical Society Australian Division. He
is now an executive consultant providing services to the aviation and broader engineering communities.
10
APISAT-2014
Lecture Title
Autonomous Multi-UAV System for Cooperative Transportation
Lecturer
Prof. Min-Jea Tahk
Affiliation
Professor, Division of Aerospace Engineering
Korea Advanced Institute of Science and Technology (KAIST)
program
KOREA
Education
Prof. Tahk received his doctor and master degree in Aerospace Engineering at The University of Texas in 1986
and 1983. He gained his bachelor degree in Aeronautical Engineering at Seoul National University in 1976.
He once worked as research scientist at Integrated Systems, Inc, USA from 1987 to 1989 and research engineer
at Agency for Defense Development, Korea from 1976 to 1981. Prof. Tahk joined KAIST Division of Aerospace
engineering in 1989 and worked as Assistant Professor from 1989-1991, Associate Professor from 1991-1999
and Professor since then.
Prof. Tahk is a Technical Editor at IEEE Tr. Aerospace and Electronic Systems since 2011 and once served as
Associate Editor there for five years before that. He has been a member of the Editorial Board, Engineering
Optimization, Taylor & Francis since 2004. During 2005 and 2011, he was an Associate Editor for Control
Engineering Practice, IFAC, Elsevier
His academic and advisory activities include:
2013.10-2015.10, Member, National Space Committee
2013-2014, President, Korea Unmanned Vehicle Systems Association (KUVS)
2012, President, The Korea Society for Aeronautics and Space Sciences (KSAS)
2010-2011, Vice President, The Korea Society for Aeronautics and Space Sciences (KSAS)
2010, Vice President, Institute of Control, Robotics and Systems (ICROS)
2009, International Program Committee Co-Chair, The 60th International Astronautical Congress, Daejeon, 2009 (IAC)
2007-2012, Vice President, Korea Unmanned Vehicle Systems Association (KUVSA)
2007-2008 Vice President, Institute of Control, Automation and Systems Engineers (ICASE)
2007-2008, Director, Society of Instrument and Control Engineers (SICE)
2007, Organizing Committee Chair, International Conference on Control, Automation and Systems (ICCAS
2007)
2004, Program Chairman, 2004 KSAS-JSASS Joint Symposium on Aerospace Engineering
JAPAN
Lecture Title
Long-Term Vision of Future Air Traffic Systems in Japan
Lecturer
Mr. Yutaka Fukuda
Affiliation
Deputy Director, Air Traffic Management Department
Electronic Navigation Research Institute
Yutaka Fukuda is the Deputy Director of the ATM (Air Traffic Management) Department at the ENRI (Electronic
Navigation Research Institute). The ENRI is responsible for research and development in the field of ATM
in Japan, supporting the JCAB (Japan Civil Aviation Bureau). He serves on CARATS (Collaborative Actions
for Renovation of Air Traffic Systems) Research and Development Promoting Subcommittee. He has studied
airborne collision avoidance system, arrival management, oceanic flexible route system, conflict management
and trajectory management after joining ENRI. He was a visiting researcher at the NASA Ames Research Center
in 1995. He received a MS degree in Electronics from Tokyo Institute of Technology in 1986 and a BS degree in
Electronics from Tokyo Institute of Technology in 1984.
11
APISAT-2014
program
Invited Lecture:September 25 Thursday 11:00-12:00
CHINA
11:00-12:00
The Concept and
Principle of Next
Generation Aircraft's
Mission System
Dr. Guoqing Wang
President,AVIC Aeronautical Radio
Electronics Research Institute
CHINA
Lecture The Concept and Principle of Next Generation Aircraft's Mission System
Lecturer
Dr. Guoqing Wang
Affiliation
President,AVIC Aeronautical Radio Electronics Research Institute
Mr. Wang Guoqing, Ph.D, research fellow. Mr. Wang graduated from Northwestern Polytechnical University,
received a doctor's degree in computer science and technology, and as doctoral tutor of Northwest Polytechnology University of China since 2000. He was the president of Aeronautic Computing Technology Research
Institute ( ACTRI) of China from 2004 to 2008. He is the president of China National Aeronautical Radio
Electronics Research Institute ( CARERI ) since 2008.
Mr. Wang’s main professional directions of are integrated avionics system，avionics system architecture,
integrated modular avionics ( IMA ) system, distributed parallel signal processors, distributed parallel processing,
high reliability fault redundant computer, and computer networks.
Mr. Wang’s major published books and papers are:
1."Civil Aircraft Avionics Systems", Shanghai Jiaotong University Press of China, 2011.
2."Date Fusion Research Of integrated Modular Avionics System", Intelligent Data Engineering International
Conference of China, 2011.
3."Integration Technology For Avionic System", the 31rd Digital Avionics Systems Conference ( DASC 31),
2012.
4."Research on the Architecture Technology for New Generation Integrated Avionics System", 2013 AIAA
Aviation
5."Research on Distribute Integrated Modular Avionics System Architecture Design and Implementation ", the
32rd Digital Avionics Systems Conference ( DASC 32), 2013.
12
APISAT-2014
program
Technical Session Program
13
Opening Ceremony at Ballroom 1+2, Addressed by Haiyan, Hu, VP of CSAA
08:30-08:45
19:00-20:30
18:25- 18:40
18:10-18:25
17: 55-18:10
17:40-17:55
17:30 -17:40
17:25-17:30
17:15-17:25
17:10-17:15
17:00-17:10
15:45-17:00
15:25 -15:45
14:40-15:25
14:30-14:40
13:30 -14:30
12:00 -13:00
11:00 -12:00
10:45-11:00
09:45-10:45
08:45-09:45
1-5 Aircraft System
Break
1-4 Aircraft Design
and Optimization 2
1-3 Aircraft Design
and Optimization 1
1-2 UAV 2
1-1 UAV 1
ROOM1
5-3 Structural
Optimization (3)
5-5 Aeronautical
Materials
Break
Reception at Ballroom 1+ 2
Mechanics2
3-5 Flight
Break
Break
5-4 Fatigue and
Fracture
Coffee Break
3-3 CFD Algorithms 1
3-4 CFD Algorithms 2
2-5 GNC of
UAV:Toward
Practical Missions
5- 1 Structural
Simulation
5-2 General Design
Break
3-2 Aerodynamic
Optimization and
Design 2
2-4 Design of
controller
2-3 Avionics
Application
2-2 Advanced
Design/Simulation
and Methods
3-1 Aerodynamic
Optimization and
Design1
2-1 Advanced
Aerodynamic
Measurement
and Visualization
Technology
ROOM 5
Lunch at Ballroom 3
ROOM 3
ROOM 2
Coffee Break
6-5 Combustion 3
Break
6-4 Combustion 2
6-3 Combustion 1
6-2 Aircraft Engine
System 2
6-1 Aircraft Engine
System 1
ROOM 6
7-5 Acoustics
Break
7-4 Experimental
Techniques and
Applications 3
7-3 Experimental
Techniques and
Applications 2
7-2 Experimental
Techniques and
Applications 1
7-1 Aeroelasticity(4)
ROOM 7
"Plenary Lecture at Ballroom 1+2 ""Development of High-Performance Structural Composites with Mutltifunctionality for Aerospace
Application"", Prof. Xiaosu Yi, Director, AVIC BIAM and AVIC Composites Center (ACC), China"
"Plenary Lecture at Ballroom 1+2: ""Asia-Pacific Air Transport - the next 20 Years"", Prof. John Vincent, University of New South Wales
Board Director of the Qantas Foundation Memorial Ltd., Australia"
On site registration outside Ballroom 1+2
07:30-08:00
8-7 Flight Quality，
Fault Diagnosis and
Tolerant Control
8-6 Control Theory
and Analysis
8-4 Guidance
Control
8-5 Guiance
Technology
8-3 Air Traffic
Management 2
8-2 Air Traffic
Management 1
8-1 Flight
Mechanics1
ROOM 8
Sep.24 Wed
program
14
APISAT-2014
18:40-18:55
18:25-18:40
18:12-18:25
18:10-18:15
18:00-18:10
17:55-18:00
17:45-17:55
17:40-17:45
17:30-17:40
17:20-17:30
17:10-17:20
17:00-17:10
16:30-16:45
16:45-16:55
16:55-17:00
16:10-16:30
16:05-16:10
16:00-16:05
15
19:00-20:30
1-10 Cooling System
1-9 Cost engineering
Break
1-8 Aircraft
Aerodynamics3
Coffee Break
15:40-15:55
15:55-16:00
1-7 Aircraft
Aerodynamics2
1-6 Aircraft
Aerodynamics 1
ROOM1
ROOM 2
ROOM 3
2-9 Target
Identification
Technique
Break
2-8 GNC of
Spacecraft
Coffee Break
3-9 Simulation
of Aerodynamic
Heating
Break
3-8 Simulation
of Unsteady
Aerodynamics
Coffee Break
5-10 Composite
Materials
Break
5-9 Jet Flows
5-8 Structural
Dynamics and
Aerodynamics
5-7 Aeronautical
Structural
Manufacture and
Test
Break
5-6 Flight
Mechanics3
ROOM 5
ROOM 6
ROOM 7
7-7 Fluid -Structure
Coupling
7-8 Flow Control 1
6-9 Spacecraft
Propulsion System 2
7-9 Flow Control 2
Break
6-8 Spacecraft
Propulsion System 1
Coffee Break
6-7 Flight Simulation
7-6 Conceptual
6-6 Turbine and Heat
Design and
Trasnfer
Evaluation Methods
Banquet at Ballroom 1+ 2
2-7 GNC of Miniature
3-7 CFD Applications
Aircraft
2
2-6 New Methods of
3-6 CFD Applications
Navigation，Estimate
1
and Tracking
Lunch at Ballroom 3
Invited lecture: Lecture title TBD, Dr. Guoqing Wang, China National Aeronautical Radio Electronics Research Institute, China
14:40-15:40
14:30-14:40
13:30-14:30
12:00-13:00
11:00-12:00
Coffee Break
8-11 Intelligent
Computing，
Communication and
Control
Break
8-10 Simulation of
Hypersonic Cases
8-9 Aerodynamic
Studies of Power
Systems 2
8-8 Aerodynamic
Studies of Power
Systems 1- 2
ROOM 8
Plenary Lecture: "Long-Term Vision of Future Air Traffic Systems in Japan", Mr. Yutaka Fukuda, Electronic Navigation Research Institute, Japan
09:45-10:45
Sep.25 Wed
program
10:45-11:00
Plenary Lecture : "Autonomous Multi-UAV System for Cooperative Transportation", Prof. Min-Jea Tahk, KAIST, Korea
08:45-09:45
APISAT-2014
DAY1
Time
Paper NO
Title
Paper ID
Session1-1 UAV 1 11:00-12:00
11:00-11:15
01-01-1
11:15-11:30
01-01-2
11:30-11:45
01-01-3
11:45-12:00
01-01-4
Calculation and Analysis on Stealth and Aerodynamics Characteristics of a
Medium Altitude Long Endurance UAV
Su Haoqin, Bao Xiaoxiang , Li Jianhua , Liu Kai, Cen Mengxi, Song Jing
The 11th Department of China Academy of Aerospace Aerodynamic, China
Development and Analysis of Project Based Learning Constructing Indoor
Unmanned Aerial Vehicle
Juri Kimura, Koji Miki, Yasuko Nakamuta, Shinji Suzuki
The University of Tokyo, Japan
Trajectory Design for Target Localization by UAVs with Bearing-Only Sensor
Jaehwan Pi , Hyochoong Bang
Korea Advanced Institute of Science and Technology, Korea
Aerodynamic Analysis of Duct Shape for VTOL Ducted Fan UAV
Minhyoung Ryu, Leesang Cho, Jinsoo Cho, Hanyang University, Korea
(68)
(283)
(297)
(325)
Session1-2 UAV 2 13:30-14:30
13:30-13:45
01-02-1
13:45-14:00
01-02-2
14:00-14:15
01-02-3
14:15-14:30
01-02-4
Arrowhead-Research on Design of Compound-UAV with Fenestron
Shen Wei, Hou Lili
Aircraft Design and Research Institute of AVIC Harbin Aircraft Industry Group
Co., LTD. China
Improving Electric Powered UAVs'Endurance by Incorporating Battery
Dumping Concept
Tan Chang, Hu Yu
Northwestern Polytechnical University, China
Development of Efficient Design Synthesis Method for High Altitude Long
Endurance UAV system
Jeong A Yang, Kwon-Su Jeon, Jae-Woo Lee and Sangho Kim
Konkuk University, Seoul, Korea
The Multidisciplinary Design Optimization Process and Design Framework
Development for the Unmanned Gliding Vehicle
Kwon-su Jeon, Maxim Tyan, Sung Hyun Jin, Seong Jun Cho, and Jae-Woo Lee
Konkuk University, Korea
(361)
(341)
(443)
(444)
Session1-3 Aircraft Design and Optimization 1 14:40-15:25
14:40-14:55
01-03-1
14:55-15:10
01-03-2
15:10-15:25
01-03-3
Design, Modeling and Analysis of a Sharp-Edge Hypersonic Stealthy Re-entry
Vehicle
Guofu Liu, Daochun Li, Jinwu Xiang, Wenli Luo
Beijing University of Areonautics and Astronautics, China
Introduction of integrated satellite design and analysis software, KARI Satellite
Design Software
Min Ki Kim
Korea Aerospace Research Institute, Korea
Behavior of tether for captive stratosphere platform using airship
Kazuhisa Chiba, Shin Satori, Ryuichi Mitsuhashi,
Hokkaido University of Science, Japan
Jun'ya Sasaki, Ryojiro Akiba, Hokkaido Aerospace Science and Technology
Incubation Center, Japan
(336)
(342)
(345)
Session1-4 Aircraft Design and Optimization 2 15:45-17:15
15:45-16:00
01-04-1
16:00-16:15
01-04-2
16:15-16:30
01-04-3
16:30-16:45
01-04-4
16:45-17:00
01-04-5
EKF Based Wind Velocity Estimation without an Airspeed Sensor for Unpowered
Gliding Vehicle
Yong-Gonjong Park, Chan Gook Park
Seoul National University, Korea
An Integrated Platform for Aircraft Conceptual Design and Optimization
Yuandong Zhao, Haixin Chen,, Yufei Zhang
Tsinghua University, China
Research on Multi-Specialty Coordination, Multi-Discipline and Multifunction
Integration Oriented Modeling and Simulation Innovation
Fan Lin Cao, Baohong Liu, YifeiYao,, Xionghua
AVIC the first aircraft institute, China
Design and Simulations of a Guide-Screw Hand-Spike Nose Deflecting
Mechanism
Handong Hu, Liangxian Gu, Xiaofeng Sun, Yifan Song, Xiangpeng Shi
National Key Laboratory of Aerospace Flight Dynamics, Northwestern
Polytechnical University, China
A Reliability Prediction method based on Simulation Analysis
Luo xuegang, China Aero-Polytechnology Establishment, China
(353)
(188)
(54)
(208)
(459)
17:00-17:15
01-04-6
A Study of Closed Loop Control of Active Technique for Helicopter BVI Noise
Reduction
KOBIKI Noboru, Shigeru SAITO, JAXA, Japan
(473)
Session1-5 Aircraft System 3 17:25-18:10
17:25-17:40
01-05-1
17:40-17:55
01-05-2
17:55-18:10
01-05-3
The Application of Tooth Contact Analysis in the Shaper Modification for
Face-gear
Canhui WU, Ping CAO, China Aero-polytechnology Establishment, China
Research on Probabilistic Safety Analysis Approach of Flight Control System
based on Bayesian Network
Chen Kang, Lu Zhong, Nanjing University of Aeronautics & Astronautics, China
Zeng Haijun, Nanjing University of Aeronautics & Astronautics, China
Research and Development Center, AVIC COMMERCIAL AIRCRAFT ENGINGE
CO., LTD., China
The Role of Electromagnetic Compatibility Qualification-Considerations in
Airborne System Integration Programs
Huiying Li, Mark Bolsover, Junhui Ye, Linfang Yan
Shanghai Aircraft Design and Research Institute, China
(59)
(349)
(430)
Session2-1 Advanced Aerodynamic Measurement and Visualization Technology 11:00-12:00
11:00-11:15
02-01-1
11:15-11:30
02-01-2
11:30-11:45
02-01-3
11:45-12:00
02-01-4
Dimensional Measurement of Small Hot Pieces Based on a Monochrome CCD
Bi Chao, Qu Xinghua, Liu Yong, Liu Yaping, Liu Jingliang
Aviation Key Laboratory of Science and Technology on Precision
Manufacturing Technology, Beijing Precision Engineering Institute for Aircraft
Industry, China
State Key Laboratory of Precision Measuring Technology and Instrument,
Tianjin University, China
Design and Calibration of a Six-axis Force/torque Sensor with Large
Measurement Range used for the Space Manipulator
Danfeng Chen, Aiguo Song, Ang Li, Southeast University, China
Research on 3D Virtual Environment Modeling Technology for Space Telerobot
Biyu Zhu, Aiguo Song, Xiaonong Xu, Song Li, Southeast University, China
Sapphire Fiber-Optic Temperature Sensor Based on Black-Body Radiation Law
Wangwei, Shi Xiaotian, Wang Ying
China Academy of Aerospace Aerodynamics, China
(37)
(96)
(100)
(122)
Session2-2 Advanced Design/simulation and Methods 13:30-14:30
13:30-13:45
02-02-1
13:45-14:00
02-02-2
14:00-14:15
02-02-3
14:15-14:30
02-02-4
The test verification design method based on rapid prototyping technology
for aero-engine
Xiao-Jie Qiu, Wen-Hua Zheng, Yu-Ting Tang, Feng Lu
AVIC aviation motor control system institute, China
The Nanjing University of Aeronautics & Astronautics, Nanjing, 210016,china
Predictive Sliding Mode Control using Feedback Linearization for Hypersonic
Vehicle
Xianlei Cheng, Peng Wang, Luhua Liu, Guojian Tang, National University of
Defense Technology, China
Prediction of Large Deformation on Wing Based on Strain Sensors for Array
Antenna Signal Compensation
Sunghyun Park, Hansol Lee, Yoon-Seon Choi In-Gul Kim, Jong-Myong Woo
Chungnam National University, Korea
Oo-Chul Jun, Agency for Defense Development, Korea
Monte Carlo Analysis for Significant Parameters Ranking in RLV Flight
Evaluation
Jie GU, Shuguang ZHANG , Baoyin WANG
Beihang University, China
(63)
(285)
(306)
(382)
Session2-3 Avionics Application 14:40-15:25
14:40-14:55
02-03-1
14:55-15:10
02-03-2
Application of Optimal Smoothing to Beamforming Tracking Data based on a
Singer Model
Junho Jeong, Gyeonghun Kim, Seungkeun Kim,
Unmanned Systems Group, Chungnam National University, Korea
Jong-Soo Choi ,Yeong-Ju Go, Jaehyung Lee,
Aerodynamics and Aeroacoustics Laboratory, Chungnam National University,
Korea
Wireless optical communication in formation flight of CubeSat using
convergent beam
Hyun Cheol Jeon, Seoul National Universit, Korea
Chan Gook Parkb ,bDepartment of Mechanical and Aerospace Engineering/
Automation and Systems Research Institute, Korea
(495)
(205)
15:10-15:25
02-03-3
Experimental application of Impoved Hilbert Huang Transform for the
detection of air-gap eccentricity in induction motors
Jihyoung Cha, Sangho Ko
Korea Aerospace University, Korea
(376)
Session2-4 Design of controller 15:45-17:00
15:45-16:00
02-04-1
16:00-16:15
02-04-2
16:15-16:30
02-04-3
16:30-16:45
02-04-4
16:45-17:00
02-04-5
Research on the New Airplane Develop System Based on 3D-Digital
Technique and Multi-Companies Collaboration
Wang QianpingFan Lin WuXuhui, AVIC the first aircraft institute, China
Anti measure noise research of Morphing wing UAV
Su Haoqin, Bao Xiaoxiang, , Shi Hongwei, Liu Kai, Song Jing
The 11th Department of China Academy of Aerospace Aerodynamic, China
Flight Control Design Using H∞ Control Method for a Single-Propeller UAV
Satoshi Kono, Kenji Uchiyama, Nihon University,, Japan
Model Predictive Flight Controller Using Prior Air Disturbance Information
Obtained By Doppler LIDAR
Seiya Miyagaki , Shinji Suzuki,University of Tokyo, Japan
Neural Network Controller Design for a Single Tilt-wing UAV
Seonghun Yoon, Seungkeun Kim and Jinyoung Suk, Chungnam National
University, Korea
(67)
(51)
(212)
(232)
(273)
Session2-5 GNC of UAV:Toward Practical Missions 17:10-17:55
17:10-17:25
02-05-1
17:25-17:40
02-05-2
17:40-17:55
02-05-3
Implication of Dynamic Unbalance to the Inertial Accelerometer Calibration
with Vibrafuge
Xue-Ming Dong, Changcheng Institute of Metrology and Measurement
(CIMM), China
Wei Guan, Xiao-Feng Meng, Science and Technology on Inertial Laboratory
of Beihang University (BUAA), China
A Moving Target Indication Algorithm Adaptable to Illuminance Variation
Using the Histogram Matching
Seung-Gyu Yun, Sangchul Lee, Sangho Ko
School of Aerospace and Mechamical Engineering, Korea Aerospace
University, Korea
Solutions to Improve Multiple Configuration Systems Resolution in Sensors
LIU Hua , DING Quanxin, Luoyang Institute of Electro-optical Equipment of
AVIC, China
ZHOU Liwei, Beijing Institute of Technology, China
(133)
(328)
(393)
Session3-1 Aerodynamic Optimization and Design 1 11:00-12:00
11:00-11:15
03-01-1
11:15-11:30
03-01-2
11:30-11:45
03-01-3
11:45-12:00
03-01-4
Supercritical Natural Laminar Flow Airfoil Optimization
Xiaoming Fang, Yufei Zhang and Haixin Chen , Tsinghua University, China
Optimal Design of High Power Centrifugal Compressor Using Multi-Objective
Genetic Algorithm
Hyun-Su Kang, Youn-Jea Kim, Sungkyunkwan Univerisity, Korea.
Numerical Study on Vortex Alleviation of Chipped Wings
Nahyeon Roh, Sejong Oh, Pusan National University, Busan, Korea
Kwanjung Yee, Seoul National University, Seoul, Korea
Effects of Trailing Edge Thickness on the Aerodynamic Characteristics of
NACA Symmetric Airfoil
Wanghyun Kim, Gimyeong Ryu, Byoungsoo Kim, Chungnam National
University, Korea
(316)
(319)
(348)
(370)
Session3-2 Aerodynamic Optimization and Design 2 13:30-14:30
03-02-1
Optimization of Suction Control on an Airfoil Using Multi-islands Genetic
Algorithm
D.J. Zhao, Y.K. Wang, W.W. Cao, P. Zhou
Beijing University of Aeronautics and Astronautics, China
(411)
13:45-14:00
03-02-2
Parameter optimization research on lift-enhancing of multi-element airfoil
using air-blowing
Yuqin Jiao, Yan Lu
National Key Laboratory of Science and Technology on Aerodynamic Design
and Research, Northwestern Polytechnical University, China
(15)
14:00-14:15
03-02-3
Study on Drag Divergence Characteristics of Supercritical Airfoil
Ruihuan LIU, Yufei ZHANG, Haixin CHEN
School of Aerospace Engineering, Tsinghua University, Beijing, 100084, China
(201)
14:15-14:30
03-02-4
Multi-Objective Aerodynamic Optimization of Supercritical Wing with a Large
Number of Constraint
ZHAO tong, ZHANG Yufei, CHEN Haixin, Tsinghua University, China
(255)
13:30-13:45
Session3-3 CFD Algorithms 1 14:40-15:25
17:00-17:15
03-04-6
Verification of a Chemical Nonequilibrium Flows Solver Using The Method of
Manufactured Solutions
Li Wang, Wei-jiang Zhou ,Chu-qun Ji
China Academy of Aerospace Aerodynamics,,China
17:15-17:30
03-04-7
Numerical Prediction of Stability Derivatives for Complex Configurations
Fangjian Wang, Lan Chen
China Academy of Aerospace Aerodynamic, China
(477)
03-03-3
A Modification technique of Collision Probability in the Direct Simulation
Monte Carlo Method
Huang Fei, Li Peng-fei,Jin Xu-hong, Liu Xiao-wen,Cheng Xiao-li
(176)
15:45-16:00
03-04-1
Design and dynamic analysis of micro-vibration isolator for Single Gimbal
Control Moment Gyro
Shenghao Shi; Dongxu Li; Qing Luo
College of Aerospace Science and Engineering, National University of
(191)
16:00-16:15
03-04-2
A 3D Anisotropic Cartesian Grid Generation Method and Its Applications in
Viscosity Flows
Xiaotian Shi, Shuai Fang, Meng Lv, Ning Hu
(215)
16:15-16:30
03-04-3
Evolutionary maintenance based on maintenance free operating period
philosophy
Ming Xu, Yueqin Wu, China Aero-Polytechnology Establishment, China
(221)
16:30-16:45
03-04-4
Influence of high-temperature air on Three-dimensional Nozzle structure
design
Bu Junhui, China Academy of Aerospace Aerodynamics, China
Liu Huaiyin, China Academy of Aerospace Aerodynamics, China
(228)
16:45-17:00
03-04-5
An Immersed Boundary Method Based on the Volume Fraction
Yuelong He, Dun Li, Shuai Liu and Handong Ma
(384)
17:10-17:25
03-05-1
Modified discrete vortex method to simulate the unsteady aerodynamics of
two-dimensional insect-like flapping wing models in hover
Anh Tuan Nguyen, Jae-Hung Han KAIST, Korea
(190)
17:25-17:40
03-05-2
Satellite Formation Flying using Low Thrusters and Solar Sail
YeerangLim, Hyochoong Bang, KAIST, Korea
(195)
17:40-17:55
03-05-3
Prediction of Projectile Trajectories Launched from Helicopter
Hyojoon Gong, Seungsoo Lee, Inha University, Korea
Jae Seong Park, Agency for Defense Development, Korea
(263)
03-05-4
Control surface characteristics of the small-scale supersonic flight experiment
vehicle (OWASHI) of Muroran-IT
Yoshihiro Suzuki, Sakae Oishi, Kazuhide Mizobata, Nobuhiro Tanatsugu
Muroran Institute of Technology, Japan
Takakage Arai, Osaka Prefecture University, Japan
(269)
15:10-15:25
(417)
Session3-4 CFD Algorithms 2 15:45-17:00
Session3-5 Flight Mechanics2 17:10-18:10
17:55-18:10
Session5-1 Structural Simulation 11:00-12:00
11:00-11:15
05-01-1
Design and simulation of long slender end mill embedded with passive
damper
Yiqing Yang, Yu Yu, Beihang University, China
(184)
11:15-11:30
05-01-2
TC4 Hollow Fan Blade Structural Optimization Based on Bird-Strike Analysis
Zeng Chuan, Jiang Xiang-hua,
School of Jet Propulsion BUAA, China
(223)
11:30-11:45
05-01-3
Six-DOF Modeling and Simulation for Generic Hypersonic Vehicle in Reentry phase
Chao Wang ,Xinyu Liu, Feng Li
China Academy of Aerospace Aerodynamics(CAAA), China
(234)
05-01-4
Test Particle Monte Carlo Simulation of Return Flux on Various geometric
surfaces due to Ambient Scatter of Outgassing Molecules
Xuhong Jin, Fei Huang, Zhi Chen, Xiaoli Cheng
(335)
11:45-12:00
Session5-2 General Design 13:30-14:30
05-02-1
Optimal WVR Air-to-Air Combat Maneuver Generation Algorithm using
Scoring Function based on Security Strategy
Hyunju Park, Dong-Wan Yoo, Min-Jea Tahk
Division of Aerospace Engineering, KAIST, Daejeon, Korea
(236)
13:45-14:00
05-02-2
Conceptual Design of Single-stage Rocket Using Hybrid Rocket by Means of
Genetic Algorithm
Masahiro Kanazaki, Tokyo Metropolitan University, Japan
Atthaphon Ariyairt, Kazuhisa Chiba, Hokkaido University of Science, Japan
Koki Kitagawa, Toru Shimada, Japan Aerospace Exploration Agency, Japan
(426)
14:00-14:15
05-02-3
Safety of Lap-Held Infants in Aircraft
Cees Bil, Adam Shrimpton, Graham Clark, RMIT University, Australia
(460)
14:15-14:30
05-02-4
Design and Optimisation of Electromagnetic Tricycle Operated in Airport
(470)
13:30-13:45
Session5-3 Structural Optimization 14:40-15:25
14:40-14:55
05-03-1
Multidisciplinary Design Optimization of Turbine Disks Based On ANSYS
Workbench Platforms
Qi Xiaodong, AVIC Commercial Aircraft Engine Co. Ltd., Shanghai, China
Shen Xiuli, BUAA, China
14:55-15:10
05-03-2
Topology Optimization Method Research on Hollow Wide-Chord Fan Blade of
a High-Bypass Turofan Engine
J. MENG, L.F. Liao, D. Li, Y. Cao, L.Y. Yang, Y.Y. Chen, ACAE, China
(111)
15:10-15:25
05-03-3
Optimal Design Aircraft Engine Mounts
Jiang Xianghua,Du Ran, BeiHang University, China
(288)
(29)
Session5-4 Fatigue and Fracture 15:45-17:15
15:45-16:00
05-04-1
16:00-16:15
05-04-2
16:15-16:30
16:30-16:45
16:45-17:00
17:00-17:15
Essential Work of Fracture of Ductile Polymer Membranes
Hongsu Bae, Kyeongsik Woo,Chungbuk National University, Korea
Hyung-Soon Cho, Jin-Ho Rho, Soo-Yong Lee, Korea Aerospace University,
Korea
Fatigue Damage Monitoring of an Aluminum Joint Specimen
Cui Ronghong, He Yuting, Jing Bo, Hou Bo, Air Force Engineering University,
China
(276)
(106)
05-04-3
Failure Analysis Of Rubbing Of The Fan Tip And Case Of A Engine
Feifei Wei, Yunyong Chen, Zhiqing WU, Lulu Chen, Jin Meng
R&D Center Dept. of Compression System, AVIC COMMERICAL AIRCRAFT
ENGINE CO.,LTD.,China
(154)
05-04-4
Statistical Approach to Determine Continuum Damage Weibull Parameters in
Laminate Composites
Kook Jin Park,Hee-jin Kang,SangJoon Shin, ,Seung Jo Kim, Seoul National
University, KOREA
Ik-hyun Choi,MinKi Kim, Korea Aerospace Research Institute, KOREA
(303)
05-04-5
Prediction of Low Cycle Fatigue Crack Growth under Mixed-Mode Loading
Conditions using
Cohesive Zone Models
YUAN Huang, LI Huan, LI Xiao,Tsinghua University, China
(468)
05-04-6
Mechanical behavior and fatigue life assessment of a metastable austenitic
stainless steel with severe plastic distortions
ZENG Wu, Beijing Institute of Technology, China
YUAN Huang, Beijing Institute of Technology, Tsinghua University, China
(469)
Session5-5 Aeronautical Materials 17:25-18:25
17:25-17:40
05-05-1
Synthesise of Polythioether and Heat Resistant Property of Polythioether
Sealants
Guo Ruiyi, Zhang Jianzheng, Wu Songhua
AVIC Beijing Institute of Aeronautical Materials, China
17:40-17:55
05-05-2
Experimental Investigation of Dynamic properties of AerMet 100 Steel
Dayong Hu , Kangpei Meng, Hanlin Jiang
Beijing University of Aeronautics and Astronautics, Beijing 100191, P. R. China
(248)
05-05-3
Experimental report on the nano-identation testing of textured stainless steel
904 L and 316 L
Changjian Geng, Liu Fang, Tong Wenwei, Han Zhenyu, Chi Qingxin
AVIC Engine Design And Research Institute, China
(13)
17:55-18:10
(173)
18:10-18:25
05-05-4
Microstructure evolution of K6509 cobalt-base superalloy for over-temperature
WEI Zhen-wei,ZHAO Wen-xia,ZHOU Jing-yi,LIU Chang-kui,ZHENG Zhen,QU Shiyu,TAO Chun-hu
AVIC Failure Analysis Center, Beijing 100095, China
Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation,
China
(414)
Session6-1 Aircraft Engine System 1 11:00-12:00
06-01-1
Patent analysis of the course of aerojet's business and the key technologies of
hypersonic
Li Yelan, Bai Yan Zhou Peng
Beijing Seahawks Science and Technology Information Institute, China
(24)
06-01-2
Support Vector with ROC Optimization Method Based Fuel Consumption
Modeling for Civil Aircraft
ZHANG Haifeng , Nanjing University of Aeronautics and Astronautics, Nanjing,
China
Wang Xu-hui , Chen Xin-feng, China Academy of Civil Aviation Science and
Technology, Beijing, China
(124)
11:30-11:45
06-01-3
Research of Model-based Aeroengine Control System Design Structure and
Workflow
Dong Zhang, Jin-zhi Lu , Lin Wang , and Jun Li
AVIC, Shenyang Engine Design and Research Institute, China
(66)
11:45-12:00
06-01-4
Review-Volcanic ash and its influence on aircraft engine components
W.R. Chen, AVIC Commercial Aircraft Engine Manufacturing Co., Ltd., ,China
L.R. Zhao, National Research Council of Canada, Aerospace, Canada
(80)
11:00-11:15
11:15-11:30
Session6-2 Aircraft Engine System 2 13:30-14:30
13:30-13:45
06-02-1
Development Strategy Study for Commercial Aero Engine Companies in
European Countries and the United States
LIU Hong-xia, ZHANG Shi-fu, LIANG Chun-hua,
AVIC Shenyang Engine Design and Research Institute, China
LIU Qi, AVIC Academy of Aeronautic Propulsion Technology, China
13:45-14:00
06-02-2
Performance Estimation for Differential Pressurization Pulse Jet Engine
Zhang Jianpeng, Qin Lizi, He Miaosheng, Beihang University, China
(451)
06-02-3
The Effect of the Inlet Total Pressure and the Number of Detonation Waves on
Rotating Detonation Engines
Song-Bai Yao, Meng Liu, Jian-Ping Wang
Center for Combustion and Propulsion, CAPT and SKLTCS, Peking University,
Beijing 100871, China
(492)
06-02-4
Research on the Influence of Reflected Shock Wave on Continuously Rotating
Detonation Engine
Liu Yu-Si, Li Yang, Wang Yu-hui, Wang Jian-ping
Centre of Combustion and Propulsion, CAPT & SKLTCS, College of Engineering
Peking University, China
(494)
06-03-1
Numerical Study of the Combustion Field in Dual-cavity Scramjet Combustor
Wang Lu, Qian Zhansen,Gao Liangjie
AVIC Aerodynamics Research Institute, China
Aviation Key Laboratory of Science and Technology on High Speed and High
Reynolds Number Aerodynamic Force Research, China
(148)
06-03-2
Atomization Performance Study of a Fuel Injector in IGC by Experimental and
Numerical Investigation
Can Ruan, Xiaoyuan Fang, Fei Xing, Xiamen University, China
Guanxing Huang, Hongzhou Ho, Cleaning Combustion and Energy Utilization
Research Center of Fujian Province, JiMei University, China
(199)
06-03-3
Effect of combustion heat release on the stability of confined boundary/
mixing-layer confluent flow
Liu Zhiyong, , Shang Qing, China Academy of Aerospace and Aerodynamics,
China
Liu Xiaoyong, Fei Lisen, Liu Fengjun, Beijing Power Machinery Institute, China
(239)
14:00-14:15
14:15-14:30
(143)
Session6-3 Combustion 1 14:40-15:25
14:40-14:55
14:55-15:10
15:10-15:25
15:45-16:00
06-04-1
Numerical Studies of Multi-cycle acetylene-air Detonation Induced by Shock
Focusing
Zhihong Zhang, Zhiqiang Li, Gan Dong
National National Key Laboratory of Science and Technology on Aero-Engine
Aero-thermodynamics, Beijing University of Aeronautics and Astronautics,
China
16:00-16:15
06-04-2
Shock tube study on auto-ignition delay of kerosene aerosol and its cracked
mixture
(401)
06-04-3
The Testing Simulation Technology Investigation on the Thermal Environment
of Engine Combustor Wall Material
Tu Jianqiang, Chen Lianzhong, Zhang Youhua
(45)
16:15-16:30
16:30-16:45
06-04-4
16:45-17:00
06-04-5
Study on the Ignition System of a Pilot Flame in a Cannon-Type-Combustor of
a Turbo-Engine
Yasuo Obikane
Mongolian University of Science and Technology, Mongolia
Experimental Study on Spectral Characteristics of Kerosene Swirl Combustion
Hyeonjae Lee, Seonghyeon Seo
Hanbat National University, Korea
(253)
(64)
(142)
17:10-17:25
06-05-1
17:25-17:40
06-05-2
Study of the Dump Diffuser Optimization for Gas Turbine Combustors
Leilei Xu, Yue Huang,Can Ruan, Peiyong Wangand Fei Xing, Xiamen University,
China
A Large Eddy Simulation Study of Flow and Mixing Characteristics in
Supersonic Combustor
Kyoo-hwan Moon, Ji-seok Hong, Hong-gye Sung, Korea Aerospace University,,
Korea
(198)
(311)
06-05-3
Analysis of the Flame Structure of Surrogate Kerosene/GOx in Laminar
Counterflows
JeongSeok Kang, JunYoung Heo, Hong-Gye Sung , Korea Aerospace
University, Korea
(337)
17:55-18:10
06-05-4
An Experimental Investigation on Combustion Characteristics of Hypermixer
Injectors-Effects of the 'Swept' Applied to Hypermixer Injector Ramps-Noritsugu
Kubo,, Sadatake Tomioka,Tohoku University, Japan
Atsuo Murakami, Kenji Kudo, Kakuda Space Center, Japan Aerospace
Exploration Agency, Japan
(449)
18:10-18:25
06-05-5
Observation of kerosene injected from a cavity into a supersonic airstream
Shengli XU, Liseng FEI
Tsinghua University, Institute of Power Machinery, China
(400)
07-01-1
The aeroelastic characteristic of a wing with preload asymmetry freeplay
Hui Zhang, Jingtao Wu
China Aircraft Strength Research Institute, China
(249)
07-01-2
Analysis of Fluid-Structure Interaction by High Velocity Impact
Hongsu Bae, Kyeongsik Woo, Chungbuk National University, Korea
In-Gul Kim, Chungnam National University, Korea
Jong-Heon Kim, Agency for Defense Development, Korea
(274)
07-01-3
Airfoil Dynamic Stall and Aeroelastic Analysis Based on Multi-Frequency
Excitation Using CFD method
Daobo huang, Jiandong Li, Yong Liu
National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of
Aeronautics and Astronautics, China
(392)
07-01-4
Development of Aeroelastic Simulation Code Using Unstructured CFD Solver
Hitoshi Arizono
Japan Aerospace Exploration Agency, Japan
Hamid Reza Kheirandish, Research Center of Computational Mechanics, Inc.,
Japan
(471)
17:40-17:55
Session7-1 Aeroelasticity 11:00-12:00
11:00-11:15
11:15-11:30
11:30-11:45
11:45-12:00
Session7-2 Experimental Techniques and Applications 1 13:30-14:30
13:30-13:45
07-02-1
Experimental estimation on the Running Time of Gun Tunnel
Ruiqu Li,, Jian Lin, Xing Chen
China Academy of Aerospace Aerodynamics,, China
(258)
13:45-14:00
07-02-2
14:00-14:15
07-02-3
14:15-14:30
07-02-4
Experimental Validation on Lift Increment of a Flapping Rotary Wing with
Boring-hole Design
CHEN Long, YAN Wanfang, WU Jianghao,
School of Transportation Science and Engineering, Beihang University, China
Dynamic Characteristics of Cryogenic Swirl Flow under Supercritical Conditions
Seongho Cho, Haisol Kim, Youngbin Yoon
An Experimental Investigation of Showerhead Film Cooling Performance on a
Turbine Blade
Zhu Xingdan, Zhang Jingzhou, Tan Xiaoming
Jiangsu Province Key Laboratory of Aerospace Power Systems, Nanjing
University of Aeronautics and Astronautics, China
(260)
(262)
(292)
14:40-14:55
07-01-1
14:55-15:10
07-01-2
15:10-15:25
07-01-3
A Wind-Tunnel Study for Drag Characterization of Speed Skating Suits
Ki-Hun Lee, In-Ki Kim, Kwang-Soo Kim, Kybeom Kwon
Korea Air Force Academy, Korea
Young-Jin Moon, Korea Institute of Sports Science, Korea
Eun-Mi Choi, Korea Research Institute for Fashion Industry, Korea
Oh-Kyung Kwon, BSG Co., Ltd. , Korea
Mi-Kyung Kim, DYETEC, Korea
Yung-Hwan Byun, Konkuk University, Korea
Aeroheating measurement on capsule model with roughness in high-enthalpy
shock tunnel HIEST
HideyukiTanno,Tomoyuki Komuro, Kazuo Sato, KasuhiroItoh
Japan Aerospace Exploration Agency, Japan
X3 reflected shock tunnel for extended flow duration
R.G. Morgan D.E. Gildfind
Centre for Hypersonics, The University of Queensland, Australia
(362)
(476)
(94)
15:45-16:00
07-04-1
16:00-16:15
07-04-2
16:15-16:30
07-04-3
16:30-16:45
07-04-4
16:45-17:00
07-04-5
New Dynamic Stability Rig for Tri-sonic Wind-Tunnel
Liu Jin, Chen Nong, Song Yuhui, Hu Jing, Xie Ke
China Academy ofAerospace Aerodynamics,China
Improving Quality of Wind Tunnel Test Data Through the MDOE
Zhang Jiang ,Ma Handong, Qin Yongming
The Optical Flow Method Research of Particle Image Velocimetry
Hong-Wei Wang, Zhan Huang , Jian Gong, Hong-Liang Xiong
Aerodynamic characterization of 'DelFly Micro' in forward flight configuration
by force measurements and flow field visualization
Shuanghou Deng, Mustafa Percin, Bas van Oudheusden
Delft University of Technology, the Netherlands
An Experimental Investigation of the Supersonic Planar Mixing Layer with Finite
Thickness
Hailong Zhang,Jiping Wu,Jian Chen,Weidong Liu
Science and Technology on Scramjet Labortatory ,National University of
(128)
(222)
(243)
(394)
(70)
Session7-5 Acoustics 17:10-18:25
17:10-17:25
07-05-1
17:25-17:40
07-05-2
17:40-17:55
07-05-3
17:55-18:10
07-05-4
Nonlinear Self-sustained Combustion instability in a Rijke-Zhao Combustor with
Three Bifurcating Branches
Dan Zhao, S. H. Li, X.Y. Li and C. Z. Ji
Nanyang Technological University, Singapore
Passive Control of Self-sustained Combustion Oscillations Using Electrical
Heaters in a T-shaped Thermoacoustic System
Dan Zhao, S. H. Li, X. Y. Li, C. Z. Ji
Nanyang Technological Universtiy, Singapore
Azimuthal instabilities in annular Chambers with flow and axial distributed heat
source
Lei Li, Dan Zhao,
Nanyang Technological University, Singapore
Xiaofeng
A combined shape and liner optimization of a general Aero-engine Intake for
tone noise reduction
S Qiu, J Y Ying
Dept. of Discipline Engineering, AVIC Commercial Aircraft Engine CO.LTD,
No.3998 South Lianhua Road, Shanghai, 201108, China
(95)
(97)
(146)
(151)
18:10-18:25
07-05-5
A frequency domain Immersed Boundary method and its application to
2-dimensional acoustic problems
A. Liang
AVIC Commercial Aircraft Engine co. ltd., China
(214)
Session8-1 Flight Mechanics 1 11:00-12:00
11:00-11:15
08-01-1
11:15-11:30
08-01-2
11:30-11:45
08-01-3
11:45-12:00
08-01-4
Experimental Study on Aerodynamic Characteristics of Ornithopter
Hiroki T Endo
Kyushu Sangyo University, Japan,
Hironori A. Fujii
Kanagawa Institute of Technology, Japan
A Study on the Trajectory Optimization of a Tiltrotor with the Tilting Rate Limit
Takahide Miyamoto,Hiroyuki Takano, Isao Yamaguchi and Takeshi Yamasaki
National Defense Academy, Japan
A New Minimum Infinity-Norm Solution: with Applications to Spacecraft
Attitude Controls
Hyungjoo Yoon, Hyun Ho Seo, Young-Woong Park, Hong-Taek Choi
Analysis of Non-uniform Inflow Models and Parameter Estimation of an
Unmanned Coaxial Rotor Helicopter in Forward Flight
Mohammad Harun-Or-Rashid, Jun-Beon Song, Young-Seop Byun, Beom Soo Kang
Pusan National University, Korea
(74)
(75)
(110)
(113)
Session8-2 Air Traffic Management 1 13:30-14:30
13:30-13:45
08-02-1
13:45-14:00
08-02-2
14:00-14:15
08-02-3
14:15-14:30
08-02-4
Research on the MOIPSO Model for Collaborative Capability-flow Allocation
in Multi-airports Terminal Area
Chen Hao, Wu Yi, Wang Zhan,
Nanjing University of Aeronautics and Astronautics, China
A Agent-based Approach to Automated Merge 4D Arrival Trajectories in Busy
Terminal Maneuvering Area
LIANG Man,
Real Time Image Haze Removal on Multi-core DSP
Linting Bai, Yongwei Wu,
Dep. of Computer Science & Technology, No.1, Tsinghua Yuan, China
Jianchun Xie, Pengcheng Wen
AVIC Computing Technique Research Institute, China
Aviation Key Laboratory of Science and Technology on Airborne and
Missileborne Computer, China
Constructing an Index of Difficulty for Air Traffic Control Using Proximity
Parameters
Sakae Nagaoka, Mark Brown
ATM Department, Electronic Navigation Research Institute, Tokyo
(34)
(81)
(99)
(310)
Session8-3 Air Traffic Management 2 14:40-15:25
14:40-14:55
14:55-15:10
15:10-15:25
08-03-1
Optimization of Approach Trajectory Considering the Constraints Imposed on
Flight Procedure Design
Tomoki Hasegawa, Takeshi Tsuchiya,
Ryota Mori
Electronic Navigation Research Institute, 7-42-23 Jindaiji-higashi-machi, Chofu,
Tokyo, 182-0012, Japan
(452)
08-03-2
Reducing Fuel Burn through Air Traffic Flow Optimisation Incorporating Wind
Models
Zena Assaad, Cees Bil, Andrew Eberhard, Matthew Moore1
RMIT University, AUSTRALIA
(461)
08-03-3
Study on Key Techniques of Aeronautical Ad Hoc Network MAC and Network
Layer
Qiming Qiu, Cheng Gong
China National Aeronautical Radio Electronics Research Institute, China;
Zheng Fang
Shanghai Jiao Tong University,, China.
(463)
Session8-4 Guidance Control 15:45-16:30
15:45-16:00
08-04-1
Design of Optimal Earth-Moon Transfer Trajectory via L1 Point Using Energy
Level Shaping Method
Jin Haeng Choi, Tae Soo No, Gyeong Eon Jeon
Department of Aerospace Engineering Chonbuk National University, Korea
(408)
16:00-16:15
16:15-16:30
08-04-2
Analysis of Lunar Lander's Necessary Thrust Force in Landing Phase.
(431)
08-04-3
Investigation of Estimation Methods for the Time-Varying Residual Magnetic
Moment
Halil Ersin Soken, Shin-ichiro Sakai
Japan Aerospace Exploration Agency (JAXA) Institute of Space and
Astronautical Science (ISAS), Japan
(433)
08-05-1
Hybrid Re-entry Guidance for Reusable Launch Vehicle
Wang Zhi, Zhang Ran, Li Huifeng
(105)
08-05-2
Mars Atmospheric Entry Guidance Design by Sliding Mode Disturbance
Observer-Based Control
Yue-Chen Huang, Hai-Yang Li, Jin Zhang, Xin Du
National University of Defense Technology, China
(251)
08-06-1
A Long-Term Analysis of the GPS Boradcast Orbit and Clock Error Variations
Mingyu Kim, Jeongrae Kim,
(332)
08-06-2
Efficient Alignment of Position Measurements with Differing Reference Frames
ChrisRAABE, NiklasBERGSTR?M,, MatoshiISHIKAWA, ShinjiSUZUKI
EmadSAAD, JohnVIAN
Boeing Research and Technology, The Boeing Company, Seattle, USA
(364)
08-06-3
Trajectory Optimization Analysis by Dynamic Programming for Operational
Feasibility Study of Supersonic Transport
Akinori Harada, Yoshikazu Miyazawab,
Kyushu University, Japan
Atsushi Ueno, Yasushi Watanabe
Japan Aerospace Exploration Agency, Mitaka, Japan
(399)
Session8-5 Guidance Technology 16:30-17:00
16:30-16:45
16:45-17:00
Session8-6 Control Theory and Analysis 17:10-17:55
17:10-17:25
17:25-17:40
17:40-17:55
Session8-7 Flight Quality, Fault Diagnosis and Tolerant Control 17:55-18:25
17:55-18:10
08-07-1
Flight evaluation of fault-tolerant control system using simple adaptive control
method
Daichi Tokunaga, Shinji Suzuki,
Kazuya Masui, Japan Aerospace Exploration Agency, Japan
18:10-18:25
08-07-2
Application Research of MRAC in Fault-Tolerant Flight Controller
Shuguang ZHANG, Yang Feng, Di Zhang
BeiHang University XueYuan Road No.37, Beijing, 100191, China
(209)
(457)
DAY2
Session 1-6 Aircraft Aerodynamics 1 13:30-14:30
13:30-13:45
01-06-1
Study of Aerodynamic Configuration Design and Wind Tunnel Test for Solar
Powered Buoyancy-lifting Vehicle in the Near-space
Guangqiang Chen, Bingyan Chen, Pengfei Li, Peng Bai, Chunqun Ji
The Institute of aerodynamics theories and application of China Academy of
Aerodynamic of Aerospace (CAAA), China
13:45-14:00
01-06-2
Aerodynamic Configuration Design of Flight Demonstrator for Real Gas Effect
Chen Bingyana, Liu Zhoua, Gong Anlong
(155)
01-06-3
The aerodynamic characteristics of micro quadrotor in hovering near walls
Yuya Yokoyamaa, Daiki Tsujia,Satoshi Kataokaa, Yuta Chonoa, Ayaka
Yashimaa, Mizue Munekataa, Hiroyuki Yoshikawa
Kumamoto University, Japan
(279)
01-06-04
Effects of the rotor blade interval on the flow field around a quad-rotor in
hovering
Daiki Tsujia, Yuya Yokoyamaa, Yuta Chonoa, Mizue Munekataa, Hiroyuki
Yoshikawa
Kumamoto University, Japan
(281)
01-07-1
Numerical investigation of configuration influence on propeller-induced noise
Minwoo Kim, Youngmin Park, and Yongwun Jung
(291)
01-07-2
Effect of Close-Coupled Canards on Longitudinal Aerodynamic
Characteristics of a Supersonic Configuration
Zhong Lei, Keisuke Takizawaa, Tokyo University of Science, Japan
Dongyoun Kwakb, Masayoshi Noguchib, Institute of Aeronautical Technology,
JapanAerospace Exploration Agency, Japan
(450)
15:10-15:25
01-07-3
Reynolds Number Effect on Vortex Dominant Flow of the SST
Configurations
Dongyoun Kwaka, Japan Aerospace Exploration Agency, Japan
Keisuke Ohirab, Ryoyu Systems Co., Japan
Ralf Rudnik, German Aerospace Center, Germany
(472)
15:25-15:40
01-07-4
The Numerical Simulation of Civil Transportation High-lift Configuration
Hao Xuan, Su Cheng, Hu Ning, Zhang weimin
(21)
01-08-1
Special Feature of longitudinal stability and control transporting short takeoff
and landing airplane with method increasing lift force
Tran The Hunga, Nguyen Quoc An
Le Quy Don Technical University, Vietnam
(116)
01-08-2
Aerodynamic Interference Caused by the Inboard Leading-Edge Flap on the
Outboard Area of the Cranked Arrow Wing
Kosuke TOYODA, Kenichi RINOIE
The University of Tokyo, JAPAN
Dongyoun KWAK, Masayoshi NOGUCHI, Japan Aerospace Exploration
Agency, JAPAN
(137)
01-08-3
Kriging-algorithm-based Aerodynamic Model for Flush Airdata System
Yibin WANG, Xueqiang LIU, Nanjing University of Aeronautics and Astronautics,
China
Ning QIN, The University of Sheffield, UK
(144)
01-09-1
System Dynamics Based Simulation Approach on Corrective Maintenance
Cost of Aviation Equipments
Liu Fang, Huang Zhaodong
Aviation Industry Development Research Center of China, China
Lianbo ZHANG, School of Astronautics, Beijing University of Aeronautics and
Astronautics, China
(241)
01-09-2
Development and Production Costs Estimating For Aviation Equipment Based
on Uncertainty Design
Huang Zhaodong, Luo Rongxuana, Aviation Industry Development Research
Center of China, China
Jin Jing, AVIC Chengdu CAIC Electronics co.,LTD, China
(240)
14:00-14:15
14:15-14:30
(10)
14:40-14:55
14:55-15:10
16:00-16:15
16:15-16:30
16:30-16:45
Session 1-9 Cost Engineering 16:55-17:25
16:55-17:10
17:10-17:25
Session 1-10 Cooling System 17:25-18:10
17:25-17:40
17:40-17:55
17:55-18:10
01-10-1
Simulation Study of Cooling System Temperature Control
Based on subsection control
WANG Jiali, Li Yanna
AVIC The First Aircraft Institute, China
(57)
01-10-2
Experimental investigation on flow characteristics of gaseous in microchannels
Zhang Kai, Zheng Guanghua, Du Fenglei
Northwestern Polytechnical University, Xi'an, China
(421)
01-10-3
Numerical Simulation and Thermal Analysis of Stratospheric Airship
Kangwen Sun, Qinzhen Yang, Yong Xie, Mou Sun, Xiaoming Chen, Beihang
University
Yang Yang, Shun Wang, China Aerospace Science and Technology
Corporation the Eighth Academy 811 institute, Shanghai, China
(455)
Session 2-6 New Methods of Navigation, Estimate and Tracking 13:30-14:30
13:30-13:45
02-06-1
13:45-14:00
02-06-2
14:00-14:15
02-06-3
14:15-14:30
02-06-4
Maneuver strategy Adaptive Target Tracking Algorithm by Integrated Kalman
Information Filtering
Ying LI, Deyun ZHOU, Hao ZHANG, Northwestern Polytechnical University,
China
A Comparison Study of Advanced Tracking Differentiator
Design Techniques
Wang Hongwei, Wang Heping, Northwestern Polytechnical University, China
Glide Path Angle Tracking Control for UAV Automatic Carrier Landing
Seokwon Lee, Hyunjin Choi, Youdan Kim, Sungwan Kimb, Seoul National
University, Korea
Jinyoung Suk, Seungkeun Kim, Chungnam National University, Daejeon,
Republic of Korea
Multilateration System Network for Locating Aircraft in a Terminal Control Area
Sanghoon Jo, Sangho Ko, Jay Kang
Korea Aerospace University, Korea.
(42)
(109)
(175)
(275)
Session 2-7 GNC of Miniature Aircraft 14:40-15:40
02-07-1
L1 Adaptive Dynamic Inversion Controller for an X-Wing Tail-Sitter MAV in
Hover Flight
Wang Jin,Song Bifeng, Wang Liguang, Tang Wei, Northwestern Polytechnical
University, China
(46)
14:55-15:10
02-07-2
Development of Large-Scale 3D Map Generation System for Indoor
Autonomous Navigation Flight - work in progress
SungTae Moon, Wesub Eom, Hyunchul Gong, Korea Aerospace Research
Institute, Korea
(293)
15:10-15:25
02-07-3
Control Strategy of Transition Flight Using MPC for QTW-UAV
Ryota Hatori, Kenji Uchiyama, Nihon University, Japan
(437)
15:25-15:40
02-07-4
Fast SLAM for MAV Using Relative Position Measurements
Ryosuke Fujiwara, Takeshi Tsuchiya,
Daisuke Kubo, JAXA, Japan
(447)
14:40-14:55
Session 2-8 GNC of Spacecraft 16:00-17:30
02-08-1
Orbit Determination of Korea Regional Navigation Satellite System Using InterSatellite Links and Ground Observations
Jungmin Choi, Chandeok Park, Sang-Young Park, Yonsei University,, Korea
(71)
16:15-16:30
02-08-2
Boost-phase Missile Autopilot Design Based on
SDRE with Adaptive Neural Networks
Jaeho Lee, Youkyung Hong, Yongwoo Lee, Youdan Kim,
Department of Mechanical and Aerospace Engineering, Seoul National
University, Korea
Gwanyoung Moon, Byung-Eu Jun, Agency for Defense Development, Korea
(172)
16:30-16:45
02-08-3
The Ascent Trajectory Optimization of Two-Stage-To-Orbit Aerospace Plane
Based on Pseudospectral Method
Jing Songa, Haoqin Su, China Academy of Aerospace Aerodynamic, China
(231)
16:45-17:00
02-08-4
Suboptimal Formation Reconfiguration of Satellites
Under Input Directional Constraints
Yasuhiro Yoshimura, Tokyo Metropolitan University, Japan
(246)
16:00-16:15
17:00-17:15
17:15-17:30
02-08-5
FUEL-OPTIMAL IMPULSIVE SATELLITE FORMATION RECONFIGURATION WITH
IMPROVED SEMI-ANALYTICAL GLOBAL SEARCH ALGORITHM
Youngkwang Kim, Sang-Young Park, Yonsei University, Korea
(202)
02-08-6
Recent Developments of Experimental Winged Rocket: Autonomous
Guidance and Control Demonstration Using Parafoil
G.Guna Surendra, K.Yonemoto, T.Matsumoto, Y.Kutsuna, K. Itakura, H.
Yamasaki, Y.Ura, M.Ichigie, Kyushu Institute of Technology, Japan
H.Tanaka, S.Ueno, T. Someya, IHI Aerospace Co., Ltd. Japan
(304)
Session 2-9 Target Identification Technique 17:40-18:10
17:40-17:55
02-09-1
A Collision Avoidance System using a LIDAR Sensor
Jingu Kim, Sua Song, Inhyun Kim, Seungkeun Kim and Jinyoung Suk,
Chungnam National University, Korea
(272)
17:55-18:10
02-09-2
Automatic Target Recognition with semi-supervised Learning in Aerial Images
Chanho Kim, Hyochoong Bang, Korea Advanced Institute of Science and
Technology, Daejeon, Korea
(375)
Session 3-6 CFD Applications 1 13:30-14:30
13:30-13:45
03-06-1
13:45-14:00
03-06-2
14:00-14:15
03-06-3
14:15 -14:30
03-06-4
Study On The Vortex Shedding Mechanism Of Coupling Combustion Stabilizer
With V-gutter and Strong Swirl Flow
Gan Dong, Zhiqiang Li and Zhihong Zhang,
National Key Laboratory of Science and Technology on Aero-Engine Aerothermodynamics,
Applying CFD Technology to Determine the Effect of Two New Designed Fan
Inlet Distortion Generators
Li Zhipeng, Lu Chao, Wu Hui, Liu Xiaopeng, Zhang Guowang,
Transition Prediction for Three-Dimensional Configurations Using a Transition
Transport Model Considering Crossflow Effect
Jeong Hwan Sa, Sang Eon Jeon, Soo Hyung Park, Konkun University, Korea
Kyung Jin Jung, Agency for Defense Development, Korea
Flow Characteristics of 2-dimensional Supersonic Nozzle According to Nozzle
Pressure Ratio
Hyun Ah Choi, Seong Hun Bae, Jeong Soo Kim, Pukyong National University,
Korea
(267)
(294)
(329)
(429)
Session 3-7 CFD Applications 2 14:40-15:55
14:40-14:55
03-07-1
14:55-15:10
03-07-2
15:10-15:25
03-07-3
15:25-15:40
15:40-15:55
Numerical simulation study on propeller slipstream interference of high
altitude long endurance unmanned air vehicle
Guangqiang,Chen Bingyan,Chen Pengfei, Li Peng Bai,Chuqun Ji, China
Academy of Aerodynamic of Aerospace (CAAA), China
Simulation of rain effects on aerodynamic performance of an airfoil
ZHANG Rui-min, China Academy of Aerospace Aerodynamics, China
A CFD based sonic boom prediction method and investigation on the
parameters affecting the sonic boom signature
Lengyan Qian Zhansen
AVIC Aerodynamics Research Institude, China
(11)
(43)
(119)
03-07-4
Applications of Overset Grid Technique to CFD Simulation of High Mach
Number Multi-body Interaction/Separation Flow
Li Xuefei,Liu Yuan,Qian Zhansen
Reynolds Number Aerodynamic Force Research, Shenyang, China
(125)
03-07-5
Investigation on Different Methods for Numerical Simulation of Propeller
Slipstream
Zhang Ying, Ye Liang, Yang Shuo, Zhu Xinglin
Chinese Aerodynamic Research Institute on Aeronautics, China
(156)
Session 3-8 Simulation of Unsteady Aerodynamics 16:05-17:20
16:05-16:20
03-08-1
Investigation of Airfoil Unsteady Aerodynamic Characteristics Based on Finite
Macro-Element and TFI Hybrid Dynamic Mesh Correction
TANG Han, GAO Zhenxun
National Laboratory of Computatioal Fluid Dynamics, Beihang University,
China
(53)
03-08-2
Numerical Simulation of Unsteady Separated Flow over a Delta Wing Using
Cartesian Grids and DES/DDES
Meng Lv, Shuai Fang, Yudong Zhang
(102)
16:35-16:50
03-08-3
High-Performance Computing of Periodic Unsteady Flow Based on Time
Spectral Method
XIE Lijun, YANG Yunjun, LIU Zhou, ZHOU Weijiang
(159)
16:50-17:05
03-08-4
Unsteady Flow Numerical Simulation of Vertical Axis Wind Turbine
Du Gang, Wu Chun Kau
BeiHang University, China
(453)
03-08-5
Coherence Mapping of Unsteady Pressure Fields on 2-Dimensional Wings
Using Unsteady Pressure-Sensitive Paint Technique
Kazuyuki Nakakita
Japan Aerospace Exploration Agency (JAXA), Japan.
(478)
16:20-16:35
17:05-17:20
Session 3-9 Simulation of Aerodynamic Heating 17:30-18:15
17:30-17:45
03-09-1
17:45-18:00
03-09-2
18:00-18:15
03-09-3
Effects of Nose and Corner Radius on Heat Transfer Rates over Axisymmetric
Blunt Body
Zhang Liang,Chen Zhi,Gong Jian,Zhang Xuejun
Study on the unsteady aerodynamic heating of the oscillating model
Hu Peng-ju, Zhang Liang,Zheng Jin-xin
Study on Correlation of Aerodynamic Heating Data of a Combination Model
SHA Xin-guo, CHEN Xing, JI Feng, SU Peng-hui
(104)
(131)
(192)
Session 5-6 Flight Mechanics 3 13:30-14:30
13:30-13:45
05-06-1
13:45-14:00
05-06-2
14:00-14:15
05-06-3
14:15-14:30
05-06-4
Aerodynamic Characteristics and Flight Capability Prediction of the Smallscale Flight Experiment Vehicle Being Developed at Muroran Institute of
Technology, Japan
Satoshi Kondo, Yoshihiro Suzuki, Kazuhide Mizobata, Ryojiro Minato, Kazuyuki
Higashino,Nobuhiro Tanatsugu,
Muroran Institute of Technology,, Japan
Aerodynamic force measurement and flow visualization for flapping micro
aerial vehicle
Tatsuya Nomura, Yuuta Torii,
Aichi Institute of Technology, Japan
Shigeru Obayashi, Yasuhumi Konishi
Tohoku University, Japan
Optimal Ascending Trajectory Design of High Altitude Long Endurance UAVs
Using Wind Modeling
Kiduck Kim, Yunju Na, Hyochoong Bang
Korea Advanced Institute of Science Technology, Korea
Donghun Lee, Hyoungsik Choi
Sangjong Lee
Inha Technical Collage, Korea
Three Dimensional Trajectory Linearization Control for Flight of Air-breathing
Hypersonic Vehicle
G. D. Zhu, Z. J. Shen
(270)
(333)
(359)
(464)
Session 5-7 Aeronautical Structural Manufacture and Test 14:40-16:10
14:40-14:55
05-07-1
14:55-15:10
05-07-2
15:10 -15:25
05-07-3
The Application Research of ID Chip for Strain Measurement in Full Scale
Aircraft Structure Strength Static Test
Jia Zuo, Gang Wang
Full scale aircraft static/fatigue structure aviation science and technology key
laboratory, Aircraft Strength Research Institute of China, China
Research of weight deduction in full-scale aircraft static strength test
Liu bing, Zhang lei, Xia feng
Key Laboratory of static and fatigue test of full scale aircraft, AVIC Aircraft
Strength Research Institute, China
A Method for modify the Thermal Stress in the Wind Tunnel
Wang Ying, Wang Wei, Bu Junhui, Chen Ding
(134)
(174)
(229)
15:25-15:40
15:40-15:55
15:55-16:10
05-07-4
Fatigue Testing and Analysis of Aircraft Structure Subjected to Aerodynamic
and Buffet Loads
Li Yixuan, Zhang Zhijun, Shao Chuang
Laboratory of Aeronautical Acoustics and Dynamics, Aircraft Strength
Research Institute, China
(355)
05-07-5
Landing Gear Ground Load Measurement and Verification Test for a Large
Passenger Jet
Kong Xiangjun, Le Ningning, Li Chunsheng, Xiao Xianbo, Lin Bo, Xu Bing
China Academy of Civil Aviation Science and Technology, China
(107)
05-07-6
U-shaped bolts fracture failure analysis
Huanping Kong, Delin LIU, Tao JIANG
AVIC Testing Innovation Cooperation, China
Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, China
(415)
Session 5-8 Structural Dynamics and Aerodynamics 16:30-17:00
16:30-16:45
16:45-17:00
05-08-1
Static and Free Vibration Analysis of Cylindrical Shells with Shear and Normal
Deformations Effects
Ngoc Doan Tran,
Anh Tuan Nguyen
Le Quy Don Technical University, Vietnam,
KAIST, Korea
(391)
05-08-2
An Approximate Method of a Composite Plate's Modal Analysis using
Modified Spatial Function
Yongha Kim, Myungjun Kim, Sangbong Lee, Kyungmin Hwang,
Graduate School of Korea Aerospace University, Korea
Jungjin Lee,
Jungsun Park
School of Aerospace and Mechanical Engineering, Korea Aerospace
University, Korea
(491)
Session 5-9 Jet Flows 17:00-17:45
17:00-17:15
05-09-1
17:15-17:30
05-09-2
17:30-17:45
05-09-3
Oscillation flow induced by underwater supersonic gas jets from a rectangular
Laval nozzle
He Miaosheng, Qin Lizi, Liu Yu
Fluid-particle Interaction and Particle Distribution in a Particle-laden Coaxial jet
Jungsoo Yoon, Youngbin Yoon
Development of Aerodynamic Design of Hypersonic Quiet Nozzles
Ruiqu Li, Junmou Shen, Jian Gong
(245)
(247)
(256)
Session 5-10 Composite Materials 17:55-18:40
17:55-18:10
05-10-1
18:10-18:25
05-10-2
18:25-18:40
05-10-2
Vibration Reduction of a Bearingless Helicopter Rotor with Composite Tailored
Couplings
YU Jin, LUO Yu, LIU Yong,
Viscoelastic Behaviors of Shape Memory Polymer Composites
O-Hyun Kwon, Hark-Inn Kim, Soo-Yong Lee, Jin-Ho Roh
Kyo-Nam Koo
University of Ulsan, Korea
Prediction of Distortion in Flanged Composite Laminates
Using Viscoelastic Models
Xiao Lin Liu, Paul Falzon
Advanced Composite Structures Australia Pty Ltd, Australia
(170)
(296)
(485)
Session 6-6 Turbine and Heat Trasnfer 13:30-14:30
13:30-13:45
13:45 -14:00
06-06-1
Evolution of Rolls-Royce air-cooled turbine blades and feature analysis
LI Xu, SUN BO, YOU Hongde, WANG Lei
(76)
06-06-2
Design Optimization of Profiled Endwall in a High Pressure Turbine Rotor
Including Rim Seal Purge Flow Effects
Hualing Luo, Huimin Tang, Shuzhen Hu, Shuaiqiang Liu
AVIC Commercial Aircraft Engine Co., LTD., China
(153)
14:00 -14:15
06-06-3
14:15-14:30
06-06-4
Study of the Pressure Drop and Thermal Performance of An Air-Air Heat
Exchanger for Aero-Engine Application
Lu Haiying, Lv Duo, Li Yi, Shen Yi
AVIC Shenyang Aero-engine Research Institute, China
Yu Xiao,
AVIC Shenyang Aero-engine Research Institute, China
National Key Laboratory on Aero-engines, Beijing University of Aeronautics
and Astronautics, China
Dong Wei
Shanghai Jiao Tong University, China
Conjugate Heat Transfer Simulation of a Thermal Barrier Coated Turbine Vane
Jinuk Kim, Jeonggyu Bak, Jinsoo Cho
Hanyang University, Korea
Youngseok Kang, Korea Aerospace Research Institure, Korea
(149)
(197)
Session 6-7 Spacecraft Propulsion System 14:40-16:10
14:40-14:55
06-07-1
Orbit Design for Approaching Multiple Space Objects in a Circular Orbit
WEI Yanyan, WANG Hongyu,
Army Aviation Institute, China
LV Zhaofu, 65529Army, China
14:55 -15:10
06-07-2
Study on algorithms of flush air data sensing system for hypersonic vehicle
Guangqiang Chen,Guidong Wang,Bingyan Chen,Weijiang Zhou,Chuqun Ji
China Academy of Aerodynamic of Aerospace (CAAA), China
(12)
15:10-15:25
06-07-3
Nine-degree of Freedom Modeling and Flight Dynamic Analysis of Parafoil
Aerial Delivery System
Yu Gang
29# Xinhua Road, Xiangyang City, Hubei Province, China
(38)
15:25-15:40
06-07-4
Morphing process research of UAV with PID controller
Su Haoqin, Bao Xiaoxiang, Shi Hongwei, Song Jing, Huang Zhan,
The 2nd Department of China Academy of Aerospace Aerodynamic, China
(58)
15:40-15:55
06-07-5
The Effect of Airflow over Mountains on Flight Safety
Chen Junping,,Wang Lixin
(211)
06-07-6
Assessment of Landing Gear Design based on the Virtual Testing and
Evaluation Methodology
Liu Hailiang, Wang Lixin,
(298)
15:55-16:10
(6)
Session 6-8 Spacecraft Propulsion System 1 16:30-17:30
06-08-1
Optimization Selection of Regulated Pressurization System Schemes for Liquid
Attitude and Divert Propulsion Systems
Lie LIU, Guo-zhu LIANG
(181)
06-08-2
Investigation on effective sampling strategy for multi-objective design
optimization of RBCC propulsion systems via surrogate-assisted evolutionary
algorithms
Tuan Quang Ho, Hideaki Ogawa, Cees Bil
RMIT University, Australia
(219)
17:00-17:15
06-08-3
Potential of ADN-based ionic liquid propellant for spacecraft propulsion
Yuichiro Ide
School of Physical Sciences,Department of Space and Astronautical Science,
The Graduate University for Advanced Studies, Japan
Takuya Takahashi, Keiichiro Iwai,
Japan Carlit Co., Ltd., Japan
Katsuhiko Nozoe
Carlit Holdings Co., Ltd., Japan
Hiroto Habu, Shinichiro Tokudome
Japan Aerospace Exploration Agency (JAXA), Japan
(343)
17:15-17:30
06-08-4
Structural Damping Effect on Deformation of Flexible Flapping Wing
Xue Dong, Song Bifeng, Yang Wenqing, Fu Peng
Northwestern Polytechnical University, Xi'an, P.R. China
(115)
16:30-16:45
16:45-17:00
Session 6-9 Spacecraft Propulsion System 2 17:40-18:40
17:40-17:55
06-09-1
Experimental Studies on AeroThermodynamic Environments of the Interaction
Area between the Wing and the Arc Board in Arc Wind Tunnel
XU Kao, CHEN Lianzhong, LIU Xiang
China Academy of Aerospace Aerodynamics, Beijing
(233)
17:55-18:10
06-09-2
18:10-18:25
06-09-3
18:25-18:40
06-09-4
Technology and Application of Identifying Dynamic Loads Based on Flight
Test Data
Chen Liebin, Jin Wei, Shi Shanglu
Chengdu Aircraft Design and Research Institute, China
Plume interference effects on cluster operations of Hall thruster system
Yudai Uyama, Takeshi Miyasaka, Katsuo Asato, Daiki Furutaa, Daichi Shimizua,
Ryota Gotoa, Mikoto Yoshidaa, Ryosuke Murakia
Gifu University, Japan
Mixing Enhancement in a RBCC Engine Operating in Hypersonic Flow
Ryosuke Nakano, Noritsugu Kubo
JAXA Kakuda Space Center, Japan
Sadatake Tomioka, Atsuro Murakamib, Kenji Kudob, Shuichi Uedab
Tohoku University, Sendai, Japan
(16)
(493)
(114)
Session 7-6 Conceptual Design and Evaluation Methods 13:30-14:30
13:30-13:45
07-06-1
13:45-14:00
07-06-2
14:00-14:15
07-06-3
14:15-14:30
07-06-4
System Design of Solar Sail Deployment and its Effect on Attitude dynamics for
Cube Satellite CNUSAIL-1
Su-A Song, Yeona Yoo, Chang-Gu Han, Soyeon Koo, Jinyoung Suk,
Seungkeun Kim
Chungnam National University, Daejeon, Republic of Korea
Surrogate Model of Aerodynamic Model toward Efficient Digital Flight
Norazila Othman, Masahiro Kanazaki
Tokyo Metropolitan University, Japan
Improved Flight Load Analysis for Light Aircraftby Using Multi-Fidelity Database
Seung-Bin Park, Nhu Van Nguyen, Sangho Kim, Jae-Woo Lee
Department of Aerospace Information Engineering Konkuk University, Korea,
Aircraft Structural Sizing and Weight Estimation Using FE-based Preliminary
Design Tool
Danbi Hong,, Wanggu Kang, Hae-Chang Lee, Dae Sung Lee,
Korea Aerospace Reasearch Institute, Korea
Seung Jo Kimb
(305)
(416)
(448)
(350)
Session 7-7 Fluid -Structure Coupling 14:40-16:10
14:40-14:55
07-07-1
14:55-15:10
07-07-2
15:10-15:25
07-07-3
15:25-15:40
07-07-4
15:40-15:55
07-07-5
15:55-16:10
07-07-6
Numerical Research on Segmented flexible airfoils considering fluid-structure
interaction
DONG Hefeng,WANG Chenxi,LI Shaobin,SONG Xi Zhen
National Key Laboratory on Aero-Engines, Beihang University., China
Study on Two-dimensional Wing Flutter Analysis by a High-order Flux
Reconstruction Method
Issei Morinaka, Koji Miyaji
Yokohama National University, Japan
Sensitive Flutter Parameters Analysis with Respect to Flutter-Free Design of
Compressor Blade
Sun Hai, Yang Lin, Li Hongxin
AVIC Shenyang Engine Design and Research Institute, Shenyang, China
Body freedom flutter of a blended wing body model coupled with flight
control system
Yingsong Gu, Zhichun Yang, Shun He
Institute of Structural Dynamics and Control, Northwestern Polytechnical
University, China
Surface recombination effects on surface friction of reentry vehicles
Miao wenbo, Huang fei, Zhang liang, Cheng xiaoli
China Academy of Aerospace and Aerodynamics,China
Aerodynamic Performance of Micro Flexible Flapping Wing by Numerical
Simulation
Yang Wenqing, Wang Liguang, Xue Dong, Song Bifeng
(445)
(182)
(189)
(194)
(244)
( )
Session 7-8 Flow Control 1 16:30-17:30
16:30-16:45
07-08-1
16:45-17:00
07-08-2
Investigation active flow to control the separation over an airfoil NACA 2415
Tran The Hung, Nguyen Minh Xuan
A Numerical investigation of the Sparkjet Actuator in Multiple-shot Mode
LV Yuan-wei, SHAN Yong, ZHANG Jing-zhou, TAN Xiao-ming
Jiangsu Province Key Laboratory of Aerospace Power Systems, Nanjing
University of Aeronautics and Astronautics, China
(86)
(158)
17:00-17:15
07-08-3
17:15-17:30
07-08-4
Prediction of Projectile Trajectories Launched from Helicopter
Hyojoon Gong, Seungsoo Lee
Inha University, Korea
Jae Seong Park
Agency for Defense Development, Korea
Numerical Study of Active Flow Control on a Vertical Tail
Shangze Li, Zhao Li, Haixin Chen and Yufei Zhang
Tsinghua University, Beijing, 100084, China
(264)
(284)
Session 7-9 Flow Control 2 17:40-18:40
Simulation of Unsteady Flow Actuation Produced by Surface Plasma Actuator
on 2-D Airfoil
Phan Minh Khang.
E-vehicle Institute, University of Ulsan, Ulsan, Korea
Jichul Shin
Department of Aerospace Engineering, University of Ulsan, Korea
Investigation onSpanwise Wall Oscillation in Turbulent ChannelFlow Based on
Reynolds Stress Model (RSM)
DUAN Dehao, ZHANG Jinbai, GAO Zhenxun
National Laboratory of Computational Fluid Dynamics, Beihang University,
China
17:40-17:55
07-09-1
17:55-18:10
07-09-2
18:10-18:25
07-09-3
Modeling of the Heat Interface of a Plasma Actuator
Yasuo Obikane, Khemedekh Lochin
Mongolian University of Science and Technology, Mongolia
(204)
07-09-4
Improvement of Deformation Measurement Performance of the SPR Camera
System using SPR Interactive Modeling and Simulation Framework
Jong-Min Yun, Hong-Il Kima, Jae-Hung Han
Department of Aerospace Engineering, KAIST, Korea
Hyuk-Jun Kwon
Agency for Defense Development, Korea
(250)
18:25-18:40
(302)
(377)
Session 8-8 Aerodynamic Studies of Power Systems 1 13:30-14:30
13:30-13:45
07-10-1
13:45-14:00
07-10-2
14:00-14:15
07-10-3
14:15-14:30
07-10-4
Numerical Study of the Leakage Flow on a Novel Turbine Blade Tip
Dengyu Jianga, Hualing Luoa, Xiang Zhanga
AVIC Commercial Aircraft Engine Co., LTD., China
The Aerodynamic Design and Investigation of Loading Distribution of a Mixed
Flow Compressor
Chen Xuanyu,, Gui Xingmin, Jin Donghai
Meng Xiangwei
China Aero-polytechlonogy Establishment, China
Influence of Geometric Scaling on Linear Cascade Aerodynamic
Performance
Chen Fen-fen, Gui Xing-min, Jin Dong-hai, Qiu Dao-bin
Beihang University,China
Study on the design of supersonic axisymmetric multicompression and quasiisentropic inlets
JIANG Yun-song, GAO Zhen-xun, JIANG Chong-wen
Beihang University, Beijing, 100191, China
(93)
(130)
(136)
(168)
Session 8-9 Aerodynamic Studies of Power Systems 2 14:40-16:10
14:40-14:55
07-11-1
14:55-15:10
07-11-2
15:10-15:25
07-11-3
15:25-15:40
07-11-4
Numerical Simulation of Direct Action Liquid Rocket Engines Hydromechanical
Flow Conteollers
Iana Bakhmet, Zhang Lihui
Effect of angle between the primary and auxiliary holes of an anti-vortex film
cooling hole
Younggi Moon, Soon Sang Park, Jung Shin Park, Jae Su Kwak
Thermal-flow Characteristics of Double-Jet Film Cooling Holes with Various
Transverse Trench Configurations
Moon-Young Cho, Youn-Jea Kim
Sungkyunkwan Univerisity, Korea.
A Numerical Study of the Flow Dynamics of Through-type Pintle Nozzles with
Large Scale Separation Flow
Ki-Yeon Jeong, Jun-Young Heo,, Hong-Gye Sungb
(193)
(313)
(326)
(354)
15:40-15:55
07-11-5
15:55-16:10
07-11-6
Experimental Study of Surge and Rotating Stall Occurring in High-speed
Multistage Axial Compressor
Changzheng LI, Siqi XU, Zhiqi HU
Analysis of aerodynamic design characteristics of Flade fan
ZENG Yueliu, WEI Yuan
National Key Laboratory of Science and Technology on Aero-Engines Aerothermodynamics,
(405)
(428)
Session 8-10 Simulation of Hypersonic Cases 16:30-18:00
16:30-16:45
07-12-1
16:45-17:00
07-12-2
17:00-17:15
07-12-3
17:15-17:30
07-12-4
17:30-17:45
07-12-5
17:45-18:00
07-12-6
Aerodynamic Design and Numerical Simulation of Over-Under Turbine-Based
Combined-Cycle (TBCC) Inlet Mode Transition
Xiang Xianhong,Liu Yuan,Qian Zhansen
Real Gas Effect on a Standard Model Electre
Junhong Li, Honglu Pan, Liang Zhang, Wenbo Miao, Zhi Chen, Xiaoli Cheng,
Numerical Study on the Stability of Hypersonic Wake Flow over Blunt body
and Global Stability AnalysisDehua Zhu,, Qing Shena, Xiangjiang Yuan
Effect of recession on the re-entry capsule aerodynamic characteristic
Xu Guowu, Zhou Weijiang, Chen Bingyan, Zhan Huiling, Yang Yunjun
Aerodynamic Design Optimization of a Kind of Reentry Capsule Based on
CFD and Multi-objective Genetic Algorithm
Wang Rong,, Chen Bing-yan, Zhang Hong-jun,
Zhou Wei-jiang, Bai Peng, Yang Yun-jun
The First Institute, China Academy of Aerospace Aerodynamics, China
Detached Eddy Simulation on Hypersonic Base Flow Structure of Reentry-F
Vehicle
Chen Zhi, Zhang Liang, Li Pengfei
(160)
(60)
(22)
(41)
(65)
(121)
Session 8-11 Intelligent Computing, Communication and Control 18:10-18:55
18:10-18:25
07-13-1
18:25-18:40
07-13-2
18:40-18:55
07-13-3
Assessment Model of the Architecture of the Aerospace Embedded Computer
Wei Han, Xiaoying Bai,
Dep. of Computer Science & Technology, China
Jianchun Xie
AVIC Computing Technique Research Institute, China
Covariance upper bound controllers considering intermittent packet losses of
control and measurement signals
Seungeun Kang, Sangho Ko
Key Techniques Research on UAV Data Link
Jinxi Li, Yongfei Ding, Zheng Fang
China National Aeronautical Radio Electronics Research Institute, China
(98)
(327)
(462)
APISAT-2014
Online registration address: apsiat2014.csaa.org.cn.
program
Registration
On-site registration location: Pullman Shanghai South Hotel Lobby
Registration fee
Member
Non-Member
Student Member
None-member Student
Early-bird registration
(Before Aug. 25,2014)
2800RMB
3100RMB
1400RMB
1700RMB
Late registration On-site registration
(Aug. 26-Sep. 16)
(Sep. 17-26)
3400RMB
4000RMB
3700RMB
4300RMB
1700RMB
2000RMB
2000RMB
2300RMB
Notes:
1.Member refers to member of the following societies:
Chinese Society of Aeronautics and Astronautics (CSAA)
The Royal Aeronautical Society (RAeS)
The Korean Society for Aeronautical and Space Sciences (KSAS)
The Japan Society for Aeronautical and Space Sciences (JSASS)
2.Registration can only be processed after payment is done. Those who finish online registration before the early or late bird registration
deadline but fail to pay can not enjoy the favored price.
3.Authors shall register and pay before the early-bird registration deadline.
4.For onsite registration, only RMB is accepted.
5.For technical visit, please register before the late registration deadline.
Registration inclusions
Ÿ Attendance at all scientific sessions
Ÿ Morning and Afternoon coffee breaks
Ÿ Materials: a symposium bag, proceedings on a CD-ROM or USB flash drive, final
program including abstracts, name badge
Ÿ Reception dinner on Sep. 24 (Except students)
Ÿ Lunches on Sep.24 and Sep.25
Ÿ Banquet on Sep.25 (Except students)
Ÿ Post tour on Sep.26 (Except students)
Students and accompanying persons can buy extra tickets for reception, banquet and post
tour at the following price:
An extra reception dinner coupon is 300 RMB.
An extra banquet coupon on Sep. 24 is 400 RMB.
An extra post tour ticket is 500 RMB.
Proceedings and Paper Publication Policy
All accepted papers will be available on a CD-ROM for communication purpose.
After the conference, the APISAT2014 proceedings will be officially published online by Elsevier
(http://www.elsevier.com/) on its journal of Engineering Procedia. The online publishing takes 8-12
weeks. Once being published, it will be indexed by the database of Scopus and Science Direct
instantly. It will also be evaluated for the inclusion of EI (the Engineering Index) and CPCI-S
(Conference Proceedings Citation Index – Science, formerly known as ISTP).
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APISAT-2014
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The publication requires 1200 RMB for each paper within 5 pages, including figures and
tables. Each extra page will require an additional 200 RMB. The payment must be made
before Aug. 25, 2014. Upon publishing in October, the author will be asked to sign a copyright
transfer declaration by Elsevier.
Foreign authors are extremely welcome to publish papers on the APISAT2014 Proceedings
to make it more international. The APISAT2010 Proceedings has already been indexed by
CPCI-S.
Oral Presentation
Each orally presented paper is assigned 15 minutes, including Q & A. Authors please
prepare Power Point for it.
Present in the morning of Sep. 24, authors should upload their Power Point files onto the
conference computer during the morning coffee break (10:45-11:00) .
Present in the afternoon, authors shall upload their Power Point files onto the conference
computer during 13:00-13:30.
Detailed arrangement of parallel sessions can be found in this program.
Methods of Payment
On-line payment
Online payment during online registration is strongly recommended. It’s convenient and quick.
Bank Transfer
Domestic authors can choose to pay through bank transfer. Please notify APISAT and your
name in the remittance information column. The commission fee shall be borne by the
remitter.
Confirmation
After payment is done, a confirmation letter will appear on the screen with the word of
“confirmed”. It means you have finished online registration successfully. Otherwise, it means
you have not finished online registration. Please print the confirmation letter and take it to the
check-in desk.
Cancellation of registration and refund
Cancellation must be received in writing no later than Sep. 5, 2014. 15% of the registration fee
will be charged as administration cost, the rest will be refunded; cancel after this date or fail to
attend, no money will be returned.
Invoice
Chinese authors can gain their invoice for both the publication fee and registration fee upon
check-in on Sep. 23, 2014.
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APISAT-2014
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Social Events
Note: Full delegates(non-student) can enjoy social events for free. Students and accompanying
persons to attend them shall buy coupons during online or on-site registration .
The reception is 300 RMB per person, banquet 400 RMB per person and post tour 500 RMB
per person.
Welcome Reception
Date: Wednesday, September 24, 2014/ 19:00 - 20:00
Venue: Ballroom 1+2, 3rd Floor, Pullman Shanghai South
Dressing code: Smart Casual
Banquet
Dressing code: Suit and tie
Experience a truly special night in Shanghai, China at Banquet. Great food will be served
accompanied by a colorful performance. We believe this event will provide you an
unforgettable evening in Shanghai. This event is admissible by a ticket included in registration
fee. Tickets are available for students and accompanying persons. Please the banquet in formal
dress.
Programme for Performance at Banquet for APISAT 2014
19:00 Commencement of performance
19:00-19:08 Opening performance: Face Changing in Sichuan Opera
19:08-19:10 Opening words of host (introduction to distinguished guests)
19:10-19:20 Peking Opera
19:20-19:28 Magic show (Latin dance & magic show)
19:28-19:30Toast
19:40
Banquet after performance
Chinese Traditional and Modern Art Performance
The art performance will be held during the Banquet. The performance will provide 30
minutes wonderful and exciting Chinese traditional and modern show.
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APISAT-2014
program
APISAT Post Tour
A post tour program will be provided for all APISAT participants and persons with additional
tickets. This event is composed of visiting the technical site as well as the well-known
sightseeing place in Shanghai on September 26 (Friday). Please be advised that the post tour
is offered free to only registered foreign participants. Students and accompanying persons who
wish to join this event should pre-register at the website with the fee.
Dressing Code: casual
Date
Sep. 26
Friday
Time
Function
Location
9:00-11:30
Technical visit to COMAC
Shanghai Aircraft Manufacturing
Center (SAMC)
Meet in front of the venue at 9:00.
Depart at 9:10 on time.
Coupon is required.
12:00-13:00
14:00-17:00
17:30-18:30
19:00-21:00
21:00
Lunch
Visit Shanghai Museum
Dinner
Cruise on the Huangpu River
Back to the hotel
Shanghai Museum
As a museum of ancient Chinese art, Shanghai Museum possesses a collection of over 1000,000
objects, about 120,000 of which are precious national-graded works of art. Its rich and highquality collection of ancient Chinese bronze, ceramics, painting and calligraphy is specially
celebrated in the world.
Founded and first open to the public in the building previously of the horseracing club at 325 W.
Nanjing Road in 1952 and then moved into the former Zhonghui Building at 16 S. Henan Road
in 1959, the museum developed very quickly in aspects of acquisition, conservation, research,
exhibition, education and cultural exchanges with other institutes. In 1992, the Shanghai
municipal government allocated to the Museum a piece of land at the very center of the city, the
People's Square, as its new site. The whole construction took three years, from August 1993 to
its inauguration on October 12th, 1996. The 29.5 meters high new building has a construction
space of 39,200 square meters. Its unique architectural form of a round top with a square base,
symbolizing the ancient Chinese philosophy that the square earth is under the round sky, is a
distinguished architectural combination of traditional feature and modern spirit. The present
Shanghai Museum has eleven galleries and three special temporary exhibition halls. It extends
warm welcome to the visitors from all over the world.
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APISAT-2014
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Huangpu River Night Cruise
The Huangpu River is the mother river of Shanghai. Nanpu Bridge, Yangpu Bridge and
Oriental Pearl TV Tower compose of a huge picture scroll. The Bund is the cultural section of
Shanghai that best represents the blending of ancient and modern influences. This renowned
waterfront district is the city's most famous landmark. Local people honor the Huangpu River
as Mother River, and as you view the lights and spectacle from the deck of your evening
cruise, you will understand why.
Between the stately colonial edifices along the Bund, the glittering skyscrapers on the eastern
shore of Pudong, and the unceasing river traffic, there is plenty to keep your eyes from ever
resting. Besides offering a privileged view of the bridges that span the Huangpu, the cruise
boats also offer an excellent view of the famous colonial-era buildings that make up the
Bund, buildings such as the Peace Hotel with its unique pyramid roof in blazing green and the
Customs House with its large clock tower.
The main ticket office of Huangpu River Cruise is opened daily, and the schedule usually
includes a full morning cruise (from 9am to 12:30pm) and a full afternoon cruise (from 2 to
5:30pm). Both these full cruises make a complete circuit of the Huangpu to its mouth. The
Huangpu River cruise company also offers a night cruise from 7 to 9pm, splendid when the
lights are on the Bund and Pudong, but this voyage does not go downriver to the Yangtze.
Cruise schedules vary depending on the season, and on weekends additional cruises are
sometimes added.
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APISAT-2014
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General Information
Conference Venue
Pullman Shanghai South Hotel
Location
To Hongqiao Airport: 15 KM
To Pudong Airport : 46 KM
To Shanghai South Station: 0.8 KM
To Caohejing High Tech Park: 3 KM
To Shanghai Stadium : 3.5 KM
To Xujiahui : 4.5 KM
To The Bund: 12 KM
Add: No. 1, Shanghai Pubei Rd. China, Post code: 200235
Tel: 021-24268888
Fax: 021-24268999
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APISAT-2014
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Transport information
1.Taxi
It takes about half an hour for a taxi to arrive at the hotel from Shanghai Hongqiao
International Airport and costs about RMB 50 (in daytime) or 70 (at night); while it takes
about one hour for a taxi to arrive at the hotel from Shanghai Pudong International Airport and
costs about RMB 160 (in daytime) or RMB 220 (at night). The above does not take any traffic
jam into consideration.
2.Subway
From Shanghai Pudong International Airport to Pullman Shanghai South
Maglev train
From
Subway line 1
Subway line 2
Taking about 2 hour and 10 minutes
Shanghai Pudong International Airport
Taking Maglev train at the airport
1 station
Getting off at Longyanglu Stop
Take Subway line 2 (in the direction to Xujingdong)
7 stops
Getting off at Renminguangchang Station
Transferring to Subway line 1 (in the direction to Shenzhuang)
410 m
Getting off at Shanghai South
Walking to Pullman Shanghai South
to
970m
Pullman Shanghai South
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APISAT-2014
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From Shanghai Hongqiao International Airport to Pullman Shanghai South
Subway Line 10
Subway Line 3 Taking about 1 hour and 10 minutes
Shanghai Hongqiao International Airport
From
Walking to the subway station at Terminal 1 of the airport
820 m
Taking Subway Line 10 (in the direction to New Jiangwan City) and getting off at the Hongqiao Road
Station
6 stations
Transferring to Subway Line 3 (in the direction to Shanghai South Railway Station) 260 m
Taking Subway Line 3 (in the direction to Shanghai South Railway Station) and getting off at the Station
for Shanghai South Railway Station (Exit 6)
5 stations
Walking to Pullman Shanghai South 1.2 km
to
3.Bus
From Shanghai Hongqiao International Airport to Pullman Shanghai South
Airport Bus Line 7
From
Shanghai Hongqiao International Airport
Walking to the airport bus station at the airport 30 m
Taking Airport Bus Line 7 and getting off at the station for Shanghai South Railway Station
Walking to Pullman Shanghai South
to
44
1.6 km
4 stations
APISAT-2014
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Accommdation　We have negotiated favored price for APISAT2014 delegates at the conference venue and a
few others with different levels around it.
Pullman Shanghai South (Conference venue)
Pullman Shanghai South is an international upscale business hotel, ideally situated in Star
Plaza, which comprises of a commercial building and a four-storey shopping mall in the new
CBD of south Shanghai.
Room type
Superior King Room
Superior Twin Room
Rate (per night)
CNY880
CNY980
Incl.
1 breakfast buffet included
2 breakfast buffet included
To reserve, please fill out the RESERVATION SHEET and return it to the hotel before Sep. 6,
2014. The sheet can be downloaded from: http://apisat2014.csaa.org.cn/pages/accommdation
We strongly recommend you to reserve early.
Other Options
NO
1
Hotel & Star
Room type
Shanghai Everbright
Standard room
Int’l Hotel
(Twin bed)
★★★★
Discount
Rate (CNY)
480
2
H . Hotel
★★★★
Standard room
(Twin bed)
450
3
JinJiang Inn(Long
Cao Road)
Standard room
(Twin bed)
269
Conference venue
10mins to Pullman on foot/ 5mins
by taxi
Service fee/breakfast/ internet
access included
15mins to Pullman on foot/ 8mins
by taxi
access included
Pullman on foot/ 10mins by taxi
access include
To reserve, please fill out the reservation sheet and return it to Beijing Wanlixing Conference Service Co., Ltd. The form can
be downloaded from http://apisat2014.csaa.org.cn/pages/accommdation
Contact: Tom Zhu and Jerry
E-mail: [email protected];
Tel: 86-10-56385301/56385348 Fax: 86-10-56385348
Mobile: 86-13439260120/13381165301
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APISAT-2014
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Currency
Local Currency
Chinese currency is called Renminbi (literally people's currency), often abbreviated as RMB.
Issued by the People's Bank of China, it is the sole legal tender for both the Chinese nationals
and foreign tourists. The unit for Renminbi is Yuan, Jiao and fen. The conversion among the
three is: 1 Yuan = 10 Jiao =100 Fen. Chinese people normally refer to Yuan as Kuai, Jiao as
Mao. RMB is issued in both notes and coins. The denominations of paper notes include 100,
50, 20, 10, 5, 2 and 1 Yuan; 5, 2 and 1 Jiao; and 5, 2 and 1 Fen. The denominations of coins
are 1 Yuan; 5, 2 and 1 Jiao; and 5, 2 and 1 Fen.
Credit cards can be accepted at most hotels, tourist shops and some department stores.
Currency Conversion
One can change money upon arrival at the international airports of Shanghai. Also most hotels
offer foreign exchange services and exchange cash and travelers cheques. The Bank of China
exchanges money and travelers cheques. In China, wherever you exchange money the same
day, the exchange rate is the same. Banking Hours: Mondays to Fridays, 9 a m to 5 pm.
Foreign Exchange
There are no quantitative restrictions imposed on foreign currencies, traveler's checks, or
credit cards brought in.
Inbound passengers carrying foreign currencies in cash of more than 5,000 U.S. dollars
should declare to the Customs. The Customs shall release it on passengers' departure upon the
declaration made at the last entry.
Without last time declaration record of foreign currencies in cash, or if the recorded amount is
less than what the passengers carry this time, the Customs shall release the discrepancies upon
certificate issued by the Foreign Exchange Bureau or its authorized banks.
RMB
The limit of RMB allowed to bring in or take out of China is 20,000 yuan.
Voltage
Electricity is supplied at 220 volts, 50 cycles
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APISAT-2014
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About Shanghai
Entering Shanghai, you will immediately be overwhelmed by the hustle and bustle of a
thriving city: itscolours, its people, its futuristic skyscrapers and indigenous Shikumen houses.
Check out this sectionbefore coming to Shanghai.
Shanghai Location
Shanghai literally means the city by the sea. Shanghai is situated at 31o14' north latitude and
121° 29'east longitude, on the west shore of the Pacific Ocean. It is bordered on the north and
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APISAT-2014
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west by Jiangsu Province , on the south by Zhejiang Province, and on the east by the East
China Sea . Right in the middle of China's east coastline, Shanghai is an excellent sea and
river port, boasting easy access to the vast hinterland. The city is divided into two parts by
the Huangpu River: Puxi (west of the Huangpu River) and Pudong (east of the Huangpu
River). Puxi is the older part of the city and hosts the majority of shops, restaurants and
museums. Pudong is the modern part, and is recognized for its rather unusual yet extremely
impressive high-rises such as Shanghai's tallest buildings, the Shanghai International
Financial Center, Jinmao Building and the Oriental Pearl TV Tower.
Shanghai Population
Due to constant inflow of people from other parts of the country, the size of population in
Shanghai keeps growing. Before Shanghai was liberated in 1949, it only had a population
of 5.2 million.According to the Shanghai Statistics Bureau, Shanghai's population of
residents with permanent residence registration had grown to 24.15 million, among which
14.25 million were long-term residents and 9.9 million were immigrants by the end of
2013.
Shanghai Weather & Climate
With a pleasant northern subtropical maritime monsoon climate, Shanghai enjoys four distinct
seasons, generous sunshine and abundant rainfall. Its spring and autumn are relatively short
compared with summer and winter. The average annual temperature is 18 degrees Celsius. The
city has a frost-free period lasting up to 230 days a year. The average annual rainfall is 1,200
millimetres (about 50 inches). However, nearly 60% of the precipitation comes during the
May-September flood season, which is divided into three rainy periods, the Spring Rains, the
Plum Rains and the Autumn Rains. The highest temperature is in July and August. For ten days
or so in these two months, the temperature can reach 35 degrees centigrade. The coldest period
is from the end of January to early February - usually during the Chinese Spring Festival. This
awfully cold period will last for about three days but it seldom snows. From March to May,
the conditions are pleasant so this is the best season for traveling. The 'Plum Rain Season' is
from mid-June to early July. From late August to the first twenty days of September, the city is
also susceptible to typhoons, none of which in recent years has caused considerable damage.
Generally you will need a light coat and sweater in spring and short- sleeved shirts in summer.
In autumn, long-sleeved shirts, sweater and coat are necessary, while sweater and overcoat are
appropriate in winter.
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Weather averages for Shanghai
Month
Jan
Feb
Mar
Apr
May
Jun
Jul
Aug
Sep
Oct
Nov
Dec
Average high °C
(°F)
8
(46)
8
(46)
13
(55)
19
(66)
25
(77)
28
(82)
32
(90)
32
(90)
28
(82)
23
(73)
17
(63)
17
(63)
Average low °C
(°F)
1
(34)
1
(34)
4
(39)
10
(50)
15
(59)
19
(66)
23
(73)
23
(73)
19
(66)
14
(57)
7
(45)
2
(36)
Precip-itation
mm
(inches)
48
(1.89)
58
(2.28)
84
(3.31)
94
(3.7)
94
(3.7)
180
(7.09)
147
(5.79)
142
(5.59)
130
(5.12)
71
(2.8)
51
(2.01)
36
(1.42)
Shanghai Tours & Sightseeing Highlights　Shanghai has lots to offer for both first-timers and re-visitors. What are the Top 20 attractions in
Shanghai? Shanghai has become a paradise for both shoppers and diners. Shanghai is studded
with restaurants from time-honored eateries to a vast assortment of restaurants serving French,
Italian and Japanese cuisine. Famous dishes from every major school of Chinese cooking are
served at old villa restaurants.
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The Bund - Shanghai Puxi Landmarks
World Architecture at the Bund
Add:Zhongshan Rd. (E1), Shanghai
The Bund is a symbol of Shanghai. The Bund has dozens of historical
buildings, lining the Huangpu River, that once housed numerous banks
and trading houses from the United Kingdom, France, the United States,
Italy, Russia, etc. The Bund houses 52 buildings of various architectural
styles such as Romanesque, Gothic,Renaissance, Baroque, Neo-Classical,Beaux-Arts, and Art Deco. The buildings are harmonious
in color and style, thus gaining the name of "Gallery of World
Architecture". When night falls and the lights are on, all the buildings are
lit with colorful lights, glistening and dazzling to the eye.
Bund Sightseeing Tunnel
Add: 300 Zhongshan Rd.(E1) (Puxi)
2789 Riverside Promenade(Pudong)
Tel: +86 21 58886000
The 646.7-m long Sightseeing Tunnel at the Bund runs from the Bund
at the end of Nanjing Rd. to the Oriental Pearl TV Tower in Pudong.
It is the first of its kind for pedestrians in China . The tunnel adopts
the internationally advanced SK system, taking 2.5-5-min.to cross the
river. The interior wall of the tunnel is decorated with changing colors.
The unmanned environmental, transparent carriages in the tunnel
provide visitors with an open view. A 6-sound-band acoustic system
accompanying the changing scenes, produces an effect on visitors of
being present personally at the scene.
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Waibaidu Bridge
Add:East Daming Rd. cross Rd. of Huangpu Rd
Spanning over Suzhou Creek, Waibaidu Bridge is a well-known bridge. It
was first built in I 855 of wood and rebuilt in I 907 in iron and steel The
bridge is 1 06.7-m long, with a load of 20 tons, a traffic lane of 11.2 m
and 3.6-m wide sidewalks on both sides. It was once the most elegant and
magnificent bridge in the city and, up to now, it is still considered one of
the symbols of Shanghai.
Huangpu River Cruise
Add:153, 219-239 Zhongshan Rd.(E2)
Tel:+86 21 63744461
The river cruise is an important traditional tourist item in Shanghai. The
Huangpu River is the mother river of Shanghai. It symbolizes Shanghai
and presents visitors with the cream of the city'S scenic sights on its
banks. Here you will have a glimpse of Shanghai's past and look into
the bright future of the city. Starting from the Bund the boat will bring
you upstream to the Nanpu Bridge, turn around downstream to the
Yangpu Bridge and all the way to Wusong Mouth, where the river meets
theYangtzi, and then turns back.
The cuise company owns different kinds of cruise ships, wharves and a
waiting lounge. The company offers boat trips to Wusong Mouth to see
the Three Layer-Water, Yangpu Bridge , Nanpu Bridge , the cuise of the
“Twin Dragons Playing with the Pearl ”, boat charter service and special
cuisse as required by tourists.
Three on the Bund
Add:3 Zhong Shan Road (E1), Shanghai
Tel:+86 21 63233355
Web:www.threeonthebund.com
Three on the Bund is a celebration of contemporary living where art,
culture, food, fashion and wellness converge to inspire a richer life.
The stunningly transformed neo-classical 1916 building is home to four
unique restaurants, the Giorgio Armani flagship store, Space by Three
private events space, Evian Spa by Three and the Shanghai Gallery of Art.
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2014 Asia-Pacific International Symposium on Aerospace Technology
preliminary
Chinese Society of Aeronautics
and Astronautics
CSAA

apisat-2014 - 2014 Asia-Pacific International Symposium on

Transcription

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