Program/Slides

WEDNESDAY 4 DECEMBER 2019
07:00-17:30 REGISTRATION OPEN
Mr Luther Cora
Welcome to Country
8.50 – 9.00 Professor Cees Bil
Opening Address
9:00 – 10:00 Professor Michelle Gee
Australian Defence Research Capability
10:00 – 10:20 Morning tea
Ballroom Gallery and Garden Terrace Gallery
Structures/Materials I Unmanned Systems I Supersonics/Hypersonics I Spacecraft I ATM/Navigation I Wind Tunnel Test I Aerospace Systems Design I Magnetohydrodynamics
Chair: Shengxi Jia Chair: Kenji Uchiyama Chair: Eric Chang Chair: Michael Spencer Chair: Seiay Ueno Chair: Yuqin Jiao Chair: Kenichi Rinoie Chair: Christopher James
10:20 – 10:40 Analysis of the Effect of Maneuvering Flight on Flexible Rotor System Dynamics
Shengxi  Jia
Northwestern Polytechnical University
CHINA
Operation Strategy of Solar-powered UAV Based on the Longest Endurance
Chunyang Wang
Northwestern Polytechnical University
CHINA
A Numerical Study of Supersonic and Hypersonic Sonic-Boom Penetration under Wavy Ocean Model
Po-Hsun Chen
The University of Tokyo
JAPAN
SpaceWire in Satellites
Bum-soo Yoo
Korea Aerospace Research Institute
KOREA
Multipoint Spectroscopic Diagnostics of Plasma Flows with Graphite Ablation in an Arc-Heated Wind Tunnel
Keisei Tsubouchi
Tokai University
JAPAN
Analysis and comparison of different models of pressure control technology in loading and unloading process of cargo airship
Peng Xiaotian
Nanjing University of Aeronautics and Astronautics
CHINA
Progress with Magnetohydrodynamics Experiments at the University of Queensland
David Gildfind
University of Queensland
AUSTRALIA
10:40 – 11:00 Effects of structural elastic vibration on longitudinal flight dynamics of flexible missile with large slenderness ratio in flight
Heng Li
Northwestern Polytechnical University
CHINA
Safety Analysis of UAV Built-in Aerial Launch
Shaojiang Zhang
Northwestern Polytechnical University
CHINA
Suppression of Pressure Oscillation in Open Cavity Using Plasma Actuators
Seungwoo Ha
Seoul National University
KOREA
Minimum-Time Maneuver of Satellite with VS-Pyramid Type
Mitsuyoshi Tsuchiya
Yokohama National University
JAPAN
Traffic Capacity Increase in Layered UTM Airspace through Traffic Rule Improvement
Ryosuke Kaida
Tokyo Metropolitan University
JAPAN
Numerical Modeling for a Detonation Driven High Enthalpy Shock Tunnel
Dr Qiu Wang
Institute of Mechanics, Chinese Academy of Sciences
CHINA
A Surrogate-assisted Dynamically Distributed Genetic Algorithm for Multi-Objective Design Optimization
Mr Junichi Sugimoto
Kyushu Institute of Technology
JAPAN
Zeeman effect in radiating magnetohydrodynamic flow
Owen Thompson
University of Queensland
AUSTRALIA
11:00 – 11:20 Effects of Pulse Detonation Aerodynamic loads on Dynamic Characteristics of Rotor System
Shengyuan Li
Northwestern Polytechnical University
CHINA
Study on Environmental Monitoring of Flooding Time using Drone and UAV
Jun Sato
Hue Industrial College
JAPAN
Large Scale Flat Plate Boundary Layer Transition in JF-12 Hypersonic Shock Tunnel
Guilai Han
Chinese Academy of Sciences
CHINA
Design of 3-DOF Ground Simulator for Small Satellites
Kenwoo Kim
Korea Aerospace University
KOREA
A Simulation Study of Alternative Route Structures for NOPAC Airspace Reconfiguration
Mark Brown
Electronic Navigation Research Institute
JAPAN
Testing a Full-Scale Hayabusa Model in a Large Expansion Tube
Andreas Andrianatos
University of Queensland
AUSTRALIA
Analysis on Aerodynamic Characteristics of Morphing Wing with Flexible Trailing Edge under the Influence of Propeller Slipstream
Peng Liao
Northwestern Polytechnical University
CHINA
Magnetohydrodynamic (MHD) Aerobraking for Venus Atmospheric Entry
Yu Shen Chia
University of Queensland
AUSTRALIA
11:20 – 11:40 Structure Reinforcement of KPLO Yoke and the Influence on Solar Array Deployment
Juwon Jeong
Korea Aerospace Research Institute
KOREA
Fundamental Wind Tunnel Tests of Fixed Wing VTOL UAV without Control Surface
Yasushi Morikawa
National Institute of Advanced Industrial Science and Technology
JAPAN
Study of Ultrasonically Absorptive Materials for Hypersonic Laminar Flow Control
Dr Peng Lv
China Academy of Aerospace Aerodynamics
CHINA
A Study on Adjacent Satellite Interference Cancellation in Dual-Contact Satellite Systems
Hong Won Park
Korea Aerospace Research Institute
KOREA
Path planning and collision avoidance for UAVs using 3D A* algorithm and artificial potential field technique
Seungchan Shin
Korea Aerospace University
KOREA
Mapping of Stagnation Conditions in Reflected Shock Tunnels
Juan R. Llobet
Tokai University
JAPAN
Optimization of an Oleo-pneumatic Shock Absorber Suitable for Subscale Aircraft
Chenhao Wei
Beihang University
CHINA
Stress Wave Force Balance Sting Design for Magnetohydrodynamic Drag Force Measurements in Expansion Tubes
Daniel Smith
University of Queensland
AUSTRALIA
11:40 – 12:00 Study on Performance Comparison of Constrained Optimization Controller for S/C Attitude Control
Jooho Park
Korea Aerospace Research Institute
KOREA
Investigation of Aerodynamic Heating under Hypersonic Flow using Coupled Flow – Thermal Analysis
Yusuke Mizuno
Tokai University
JAPAN
Cooperative Path Planning for Microsatellite  Cluster Approaching Space Failure Targets at Close Range
Chenggang Hou
Northwestern Polytechnical University
CHINA
Demonstration of Trajectory Based Arrival Management through Air Traffic Control Simulation
Eun-Mi Oh
Korea Aerospace Research Institute
KOREA
A Design of Evaluation Wind Tunnel for Aerodynamic Performance of Drone and UAV
Yasuo Obikane
Hue Industrial College
JAPAN
Development of Morphing Wings Driven by Antagonistic Shape Memory Alloy Wires
Hiroki Koga
Meijo University
JAPAN

 

12:00 – 13:00

Lunch
Ballroom Gallery and Garden Terrace Gallery

13:00 – 14:00 PLENARY PRESENTATION
Dr Kazuomi Yamamoto
A Flight Demonstration Project for Airframe Noise Reduction Technologies, FQUROH*Chair: Professor Koji Miyaji
14:00 – 14:10

Ingo Jahn
Welcome Reception Sponsor

Structures/Materials II Unmanned Systems II Supersonics/Hypersonics II Spacecraft II ATM/Navigation II Wind Tunnel Test II Aerospace Systems Design II
Chair: Xu Yingjie Chair: David Park Chair: Daniel Smith Chair: David Gildfind  Chair: Mark Brown Chair: Taro Imamura Chair: Willem Anemaat
14:10 – 14:30 Evaluation of Aircraft Joint Coupon Testing for Investigation of the Effect of Corrosion Inhibiting Compounds on Fatigue Life
Rachelle Ferber
University of Adelaide
AUSTRALIA
Dynamic Surface Control Approach For UAV Firefighting System
Naoto Munakata
Nihon University
JAPAN
Studying Post-Shock Relaxation using a Mach Disk
Steve Apirana
University of Queensland
AUSTRALIA
Performing Earth Observation Missions using Micro and Small Satellites
Hungu Lee
Satrec Initiative
KOREA
Path-Tracking Control of Reusable Launch Vehicle Using LQ Output Feedback Control
Woosung Cho
Korea Aerospace University
KOREA
Investigation on Deformation and Aerodynamic Characteristics of the Passive Morphing Airfoil using Low Speed Wind Tunnel
Taro Imamura
The University of Tokyo
JAPAN
Effects of design parameter on acoustic characteristics and their damping of a thruster chamber
 Jianxiu Qin
China Academy of Aerospace Aerodynamics
CHINA
14:30 – 14:50 Damage Tolerance Study on Longitudinal Cracked Stiffened Panel under Pressurized Load
An Chen
Avic Aircraft Strength Research Institute
CHINA
Comprehensive Analysis and Optimized Design of Multirotor type UAVs
Hyeongseok Kim
Seoul National University
KOREA
Unstable modes in compressible wall-bounded mixing layers
Zhiyong Liu
China Academy of Aerospace Aerodynamics
CHINA
On-orbit Image Collection Re-planning Method for Earth Observation Satellites
Seonho Lee
Korea Aerospace Research Institute
KOREA
Pilot-in-the-Loop Simulation of a Robust C* control law
Katsunori Tonogaki
The University of Tokyo
JAPAN
Detecting Shock Arrival in Expansion Tubes and Shock Tunnels Using High Frequency Photodiodes
Christopher James
University of Queensland
AUSTRALIA
2-D Study of Buffet Control on Struct-Braced Wing Aircraft using Tangential Blowing
Shiyu Li
Tsinghua University
CHINA
14:50 – 15:10 Vibration Modelling and Analysis of Aviation Integrated Circuit High Performance Manufacturing Platform
Yupeng LI
Beihang University
CHINA
Mixed Logical Dynamical Modelling of UAV Cluster Controlled by Decentralized Law
Ryotaro Saito
National Defense Academy
JAPAN
Numerical Simulation Method of Supersonic Free Shear Layer
 Zhen Gao
China Academy of Aerospace Aerodynamics
CHINA
New Force Measurement System for Satellite Vibration
Jong-min Im
Korea Aerospace Research Institute
KOREA
Optimal Trajectory of S4 for Reducing Sonic Boom Loudness
Hirokazu Suzuki
Japan Aerospace Exploration Agency
JAPAN
The X3R reflected shock tunnel: A new, long-duration operating mode for the X3 expansion tube
Samuel Stennett
University of Queensland
AUSTRALIA
Multi-objective Aerodynamic Optimization Based on an Efficient Multi-output Surrogate
 Huiqin Yao
Northwestern Polytechnical University
CHINA
15:10 – 15:30 Dynamic Characteristics of Semi-infinite Pipelines in Pressure Measurement
Chenchen Wang
Changcheng Institute of Metrology and Measurement
CHINA
UAV control and track simulation in the wake field of air recycling
Hang Zhao
Northwestern Polytechnical University
CHINA
Study on Flameholding Characteristics in a Supersonic Combustor with Different Injector Diameters
Li Jianping
Northwestern Polytechnical University
CHINA
Development of CubeSats for CANYVAL-C mission in formation flying
Geuk-Nam Kim
Yonsei University
KOREA
The Impact of Wind Forecast Uncertainty on Fuel Consumption and Optimal Aircraft Trajectory
Kazunori Suzuki
The University of Tokyo
JAPAN
Application of Tomographic Rainbow Schlieren for Square Underexpanded Jets
Yuya Hara
University of Kitakyushu
JAPAN
A Deep Learning Approach to Surrogate Modelling of Missile Aerodynamic Performance
Roy Hartfield
Auburn University
UNITED STATES
15:30 – 15:50 Research on Laser Additive Manufacturing Technology of TiC Particles Reinforced Inconel 718 Composites
Bingqing Chen
Beijing Institute of Aeronautical Materials
CHINA
A Distributed Task Allocation Algorithm for Heterogeneous UAVs with Constraints on Limited Capacity and Critical Tasks
Mi Yang
Northwestern Polytechnical University
CHINA
Concentration and Velocity Field of Supersonic Fuel Mixing by using LIF and PIV Method
Takakage Arai
Osaka Prefecture University
JAPAN
An Experimental Study on the Dynamic Material Properties for a Solid Propellant under a High Strain Rate Loading Using Low-Velocity Impact Test
Jaemin Hwang
Chungnam National University
KOREA
Study on Flight Time Variation of Continuous Descent Operation with Numerical Weather Prediction Wind Data
Masakazu Hasebe
Yokohama National University
JAPAN
Experimental Study on Full Coverage Film Cooling Characteristics of Turbine Guide Vane with Shaped Hole
Bolun Zhang
Northwestern Polytechnical University
CHINA
Dynamic Balancing Design Simulation for Certain Type of Satellite antenna
Hanyu Yao
Northwestern Polytechnical University
CHINA
15:50 – 16:10 Afternoon tea
Ballroom Gallery and Garden Terrace Galley
Structures/Materials III Unmanned Systems III Propulsion Systems I Spacecraft III ATM/Navigation III Aerodynamics I Aerospace Systems Design III
Chair: Chen Bingqing Chair: Takehiro Higuchi Chair: Christopher James Chair: Spangchui Lee Chair: Mark Brown Chair: Koji Miyaji Chair: Felix Finger
16:10 – 16:30 Strain rate effects on the mechanical behavior of as-fabricated, selective laser melted 17-4 PH stainless steel
Tyler LeBrun
Osaka University
UNITED STATES
Performance Improvement through Integrated Configuration-Control Optimization for Unmanned Tailless Aircraft
Jisoo Kang
Inha University
KOREA
Effect of Mainstream Swirling on Cold Flow Pattern of an Outer-Cavity Trapped Vortex Combustor
Dr Yi Jin
Nanjing University of Aeronautics and Astronautics
CHINA
Effect of Gas Entrainment on Performance of a Small Turbopump for Rocket Engine
Dr Soonsam Hong
Korea Aerospace Research Institute
KOREA
Experimental Comparison Of Loosely Coupled INS/GPS Land Vehicle Navigation System With Adaptive Schemes
Woo Jung Park
Seoul National University
KOREA
Gust Alleviation using Preview Controller for a Flexible Aircraft Model
Kento Fujita
The University of Tokyo
JAPAN
Comparison of Aerodynamic Design Tools for Distributed Propulsion Aircraft
Willem Anemaat
DARcorporation
UNITED STATES
16:30 – 16:50 2D-C/SiC tensile damage pattern recognition based on  acoustic emission signal clustering analysis
Dr Yongzhen Zhang
Northwestern Polytechnical University
CHINA
Unmanned Aerial Vehicle Flight Control Based on Total Energy Control System
Hang Zhao
Northwestern Polytechnical University
CHINA
Development of Flight Dynamic System for Interferometric Mission of SAR Satellite
Jae-cheol Yoon
Korea Aerospace Research Institute
KOREA
Proportional Navigation Augmented with Uncertain-Autopilot-Lag Compensation
Takeshi Yamasaki
National Defense Academy of Japan
JAPAN
Acoustic Propagation Prediction Using the Inhomogeneous Wave Equation on the Cartesian Grid
Tomoaki Ikeda
Japan Aerospace Exploration Agency
JAPAN
Equipment Contribution Rate Evaluation Method Based on RIMER and PCA
Junwen Ma
Northwestern Polytechnical University
CHINA
16:50 – 17:10 Hybrid Polyurethane Foam/ Aramid Shielding Bumper for enhanced Hypervelocity Impact Protection
Sarath Kumar Sathish Kumar
Korea Advanced Institute of Science and Technology
KOREA
Formation Distortion Compensation System for Swarming Unmanned Aerial Vehicles
Myunggun Kim
Unist
KOREA
Numerical Simulation of the Effects of a Single Laser Spark on the Dynamics of a Hydrocarbon Fuelled Scramjet Combustor
Fabian Rogg
RMIT University
AUSTRALIA
Influence of the heat shield separation distance on the aerodynamic performances of Mars probe
Junfei Wu
China Academy of Aerospace Aerodynamics
CHINA
Three-Dimensional Optimal Waypoint Guidance Based on Parameter Optimization
Jeong-Hun Kim
Inha University
KOREA
Adaptive Forward-Backward Selection Method for Sparse Polynomial Chaos Expansion
Huan Zhao
Northwestern Polytechnical University
CHINA
An Auxiliary Intake Design for Top-Mounted Inlet
Fangliang Liu
Shenyang Aircraft Design & Research Institute
CHINA
17:10 – 17:30 Design and Numerical Analysis of a New Type of Film Cooling Hole
Jia-jia Niu
Northwestern Polytechnical University
CHINA
Three-Dim-Lagrange Dynamics on Arresting Gear for UAV
Yasuo Obikane
Hue Industrial College
JAPAN
Effect of the number and distribution of diaphragms on regression rates of solid Fuel in the Hybrid rocket motor
Yihua Xu
Nanchang Hangkong University
CHINA
Multidimensional effects and self-absorption on spectroscopic observations of Saturn entry radiation
Yu Liu
University of Queensland
AUSTRALIA
MPC based 2D Path Planning for Obstacle Avoidance in Point Cloud Environment
Hyungjoo Ahn
Korea Advanced Institute of Science and Technology
KOREA
CFD Simulation of an Ejector-Jet Engine
Hiromu Inoue
Okayama University
JAPAN
Gust Response Analysis for Early Design of Advanced Air Vehicle Concepts
Roy Hartfield
Auburn University
UNITED STATES
17:30 – 17:50 Experimental Investigation on Film Cooling Characteristics of Turbine Shroud in Different Circumferential Film Hole Using PSP Technique
Dapeng Liang
Northwestern Polytechnical University
CHINA
Flying-Wing Type UAV Design Optimization By Incorporating Flight Stability Constraints
Dong-gyu Seong
Konkuk University
KOREA
Spray Characteristics of Throttleable Pintle Injector
Suji Lee
Seoul National University
KOREA
Contingency Operations Design for Korea Pathfinder Lunar Orbiter
Dr Moon-jin Jeon
Korea Aerospace Research Institute
KOREA
Navigation of an Omnidirectional Mobile Rover Using EKF-SLAM Combined with ESO
Ushio Shimomura
Nihon University
JAPAN
Skin-Friction Drag Reduction in the Turbulent Boundary Layer Based on Steady Blowing from Streamwise Slots
 Yu Bai
Northwestern Polytechnical University
CHINA
Propeller Design Framework using Open Source Tools
Willem Anemaat
DARcorporation
UNITED STATES
17:50 – 18:10 Vision-based Object Tracking Guidance of a Multirotor UAV using Deep Reinforcement Learning
Seongheon Lee
Korea Advanced Institute of Science and Technology
KOREA
Numerical Simulation of Damping Characteristic and Flow Instability Induced by Damper implementation in Solid Rocket Motor
Lei Han
Beijing Institute of Technology
CHINA
An Optimization Method of Satellite Thermal Test Based on Error Spectrum Method
Ruoji Zhang
Nanjing University of Aeronautics and Astronautics, Nanjing
CHINA
Flight Demonstration of an Airborne Coherent Doppler Lidar
Hamaki Inokuchi
Japan Aerospace Exploration Agency
JAPAN
Energy-based Conceptual Design of Battery-Powered eVTOL Aircraft for Air Ambulance Services in China
Xu Zou
Northwestern Polytechnical University
CHINA
18:30 : 20:30 Welcome Reception
Pool Peroda Marriott Hotel

 

THURSDAY 5 DECEMBER
07:00 – 09:00 REGISTRATION OPEN
09:00 – 10:00 PLENARY PRESENTATION                                                             
Professor Weihong Zhang
On the advance of optimization methods for aerospace structures integrated design and cutting processChair: Professor Junchen Yao   
10:00 – 10:20 Morning tea
Ballroom Gallery and Garden Terrace Galley
Structures/Materials IV Unmanned Systems IV Propulsion Systems II Aerodynamics II Thermal Analysis Aerospace Systems/Sensors I Aerospace Systems Design IV
Chair: Zhang Weihong Chair: David Park Chair: Roy Hartfield Chair: Falk Goetten Chair: Pan Tianyu Chair: Jeremy Anderson Chair: Sun Gang
10:20 – 10:40 Investigation of SiC Ablation Mechanism using Reaxff Molecular Dynamic Simulation
Taehoon Park
Seoul National University
KOREA
Development of Towed-Type Multi-rotor with Fixed Stabilizers
Daichi Aoki
Yokohama National University
JAPAN
Experimental and Numerical Study on working characteristics of U-shaped pulse detonation combustor
Lingyi Wang
Northwestern Polytechnical University
CHINA
Longitudinal vortex mechanism for producing the steady lift-force on a circular cylinder in a uniform flow: Effects of the geometrical parameters
Withun Hemsuwan
Suranaree University of Technology
THAILAND
Effect of Convection Time on Combustion Instability in a Single Element Combustor
Jinhyun Bae
Seoul National University
KOREA
Study on light-off characteristics of Oxygen Consumption Based Inerting Reactor
Dr Feng Shiyu
Nanjing University of Aeronautics and Astronautics
CHINA
A Comparison Study between Using Stiff Boundary Conditions and Throttle Model for Rotating Stall Process Investigation
Dapeng Liang
Northwestern Polytechnical University
CHINA
10:40 – 11:00 Numerical Study on the Effects of Varying Chevron Shaped Ribs on Film Cooling for Trailing Edge
Lin Ye
Northwestern Polytechnical University
CHINA
Finding Optimal Formation of UCAVs for SEAD Mission
Wonik Seo
Inha University
KOREA
Optimization of a Vane-Type Pre-swirl Nozzle and Comparing the Performance at the Off-design Conditions
Jungsoo Lee
Hanyang University
KOREA
Behaviors of Vortices Emitted from the Laminar Separation Bubble near Airfoil Stall When Leading-edge Is Vibrated Actively
Kento Kato
The University of Tokyo
JAPAN
Numerical Study on Heat Transfer Characteristics of  Array Impingement with Initial Cross-Flow
Tianliang Zhou
Northwestern Polytechnical University
CHINA
Theoretical study on on-ground performance of a low temperature controllable oxygen consumed catalytic inerting system
 Jun Pan
Nangjing Engineering Institute of Aircraft Systems,  Aviation Industry Corporation of Chian
CHINA
Aerodynamic/Stealth Airfoil Optimization Based on Discrete Adjoint Equation of Method of Moments
Lin Zhou
Northwestern Polytechnical University
CHINA
11:00 – 11:20 Experimental Study on Damage rule of Ti-6Al-4V under High Speed Sand Erosion
Cheng Yan
Nanjing University of Aeronautics and Astronautics
CHINA
Preliminary Study on Aerodynamic Design of  Wing-Tip-Chained Airplanes for Mars Exploration
Yoichi Suenaga
The University of Tokyo
JAPAN
Experimental and numerical Investigation of the Installation Effect on hot Jet Noise
He Jingyu
China Academy pf Aerospace Aerodynamics
CHINA
Unsteady Aerodynamic Characteristics of NACA0012 Wings with Various Aspect Ratios at Low Reynolds Numbers
Hoang Anh Nguyen
National Defense Academy of Japan
JAPAN
On the effect of thermal-diffusive instability on turbulent premixed flames
Dr Wu Jin
Nanjing University of Aeronautics and Astronautics
CHINA
Application Progress and Prospect of Optical Fiber Sensing in Aircraft Structural Health Monitoring
Jingfeng Xue
Chinese Aeronautical Establishment
CHINA
Aeroelasticity and Flight Dynamics Simulation Program: Level Flight Performance Comparison
Jaehyun Jin
Sunchon National University
KOREA
11:20 – 11:40 Mechanical Properties and Residual Stress characteristics in Titanium Alloy Fabricated by Laser Additive Manufacturing
Dengke Dong
Avic Aircraft Strength Research Institute
CHINA
External Environment Estimation of Drone for Wall Collision Avoidance
Soshi Okada
Kanazawa University
JAPAN
Hydrogen-based Flameless Gas Turbine Combustor
Farid Christo
Deakin University
AUSTRALIA
An Experimental Investigation of Flow Induced Pressure Oscillations in Rectangular Cavities
Caroline Hamilton Smith
The University of Sydney
AUSTRALIA
Thermal Analysis of Metal Additive Manufacturing Process with Consideration of Density Change
Seon Ho Jeong
Inha University
KOREA
Application of Mach-Zehnder Interferometers for Oscillating Shock Trains
Masahito Nakano
The University of Kitakyushu
JAPAN
Weapon-Target Assignment problem with interference constraints using mixed-integer linear programming
Minkyu Shin
Korea Advanced Institute of Science and Technology
KOREA
11:40 – 12:00 Impact Failure Behaviour of Two-Dimensional Triaxially Braided Composites
Yulong Li
Northwestern Polytechnical University
CHINA
Simulation Research on Attitude and Position Solution of Multi-rotor UAV Based on Virtual Multi-sensor
Xiao-min Zhang
Northwestern Polytechnical University
CHINA
Numerical study on film cooling performance of convergent-divergent nozzle
Feng Liu
Northwestern Polytechnical University
CHINA
Very-large eddy simulation of swirling nonreactive and reactive turbulent flow
Xingsi Han
Nanjing University of Aeronautics and Astronautics
CHINA
Study of Heat Transfer Characteristics of Single-Jet Impingement on Leading Edge of Sharp Cone
Zhiping Li
Northwestern Polytechnical University
CHINA
RAR Compensation by Genetic Algorithm based SAR Antenna Beam Forming
Jung-Hoon Keum
KARI
KOREA
A New High-Accuracy Attitude Algorithm Under Coning Base Motion
Li-juan Xiong
Nanchang Hangkong University
CHINA
12:00 – 13:00 Lunch
Ballroom Gallery and Garden Terrace Galley
13:00 – 14:00 PLENARY PRESENTATION                                                                                                     
Dr Wang-Gu Kang
Current Research Activities and Future Plans on Unmanned Aerial Vehicles in Korea, focused on drone with 5G network & Autonomy
Chair: Professor Kwanjung Yee    
Structures/Materials V Unmanned Systems V Propulsion Systems III Aerodynamics III Aerospace Operations I Aerospace Systems/Sensors II Aerospace Systems Design V
Chair: Justin Fox Chair: Takehiro Higuchi Chair: Farid Christo Chair: Wang Yankui Chair: Scarlett Pollock Chair: Kai Peng Chair: Seiya Ueno
14:00 – 14:20 The Effect of Fiber Volume Fraction Non-Uniformity and Resin Rich Layer on Buckling Load of Cylindrical Composite Lattice Structures
Seung-Taek Kong
Chungnam National University
KOREA
System identification of multi-copter UAV using biased-relay input and adaptive extended Kalman filter
Sangheon Lee
Ulsan National Institute of Science and Technology
KOREA
The Effect of Mainstream Turbulence Intensity on the Film Cooling Performance of the Cylinder and Shaped Hole on a Turbine Vane
Chunyi Yao
Northwestern Polytechnical University
CHINA
Numerical study of unsteady flow over a frigate in motion state
Tong Li
Nanjing University of Aeronautics and Astronautics
CHINA
Variable Fidelity Aerodynamics DB Accuracy Enhancement using CFD for F-16 6 DOF Virtual Flight Certification
Nadhie Juliawan
Konkuk University
KOREA
CubeCMG: a Variable Speed Control Moment Gyroscope for small satellites
Heok June You
Korea Aerospace University
KOREA
Design And Simulation Of The Control Excitation System
Jianghua Wang
Science and Technology on Rotorcraft Aeromechanics Laboratory, Chrdi
CHINA
14:20 – 14:40 Ultrasonic nondestructive testing technology of compression moulded Composites
Tianhang Fu
Avic Compositecorporation Ltd.
CHINA
Investigation of the combustion model on the UAS intermittent combustion engine application
Sanguk Lee
Kaist
KOREA
Superposition Prediction of Cooling Effectiveness of Dustpan-shaped Hole on Turbine Vane
Zhi-peng Xu
Northwestern Polytechnical University
CHINA
Research on Correction of wall interference for airfoil dynamic experiment based on Computational Fluid Dynamics
Professor Yuqin Jiao
Northwestern Polytechnical University
CHINA
Effect of Supplemental Air System on Ground Performance of Oxygen Consumption Inert System for Fuel Tank of Aircraft
Peng Xiaotian
Nanjing University of Aeronautics and Astronautics
CHINA
A Comparison Between Non-Adaptive and Adaptive Flight Control Systems and Addressing Potential Research Areas
Ryoichi Takase
The University of Tokyo
JAPAN
Flight Control Design using Incremental Nonlinear Dynamic Inversion and Smoothing Estimation
Tito Jehu Ludeña Cervantes
Gyeongsang National University
KOREA
14:40 – 15:00 An Experimental Investigation of Dynamic Stability of Bearingless Model Rotor Mounting Test Bench
Yan Zhu
China Helicopter Research & Development Institute
CHINA
Unsteady Aerodynamics of Flying Birds in Formation Flight
Cheolheui Han
Korea National University of Transportation
KOREA
Effect of Unsteady Wake on Turbine Blade Film Cooling along the Suction Surface Using PSP Technique
Dao’en Zhou
Northwestern Polytechnical University
CHINA
A Review of Guidelines and Best Practices for Subsonic Aerodynamic Simulations using RANS CFD
Falk Goetten
RMIT University
GERMANY
An Operational Loop Simulation Method for System of Systems Effectiveness Evaluation
Honghao Yuan
Aviation Industry Development Research Center of China
CHINA
Numerical Study and Analysis the Effect of Oil Scoop Blade Tip Shape on Oil Capture Efficiency for an Under-race Lubrication System
Le Jiang
Northwestern Polytechnical University
CHINA
Aero-Propulsive Analysis and Flight Simulation for Early Design of Advanced Air Vehicle Concepts
Roy Hartfield
Auburn University
UNITED STATES
15:00 – 15:20 Certification by analysis technology for civil aircraft structures and its application
Shihui Duan
Aviation Industry Corporation of China
CHINA
Development and Flight Test for Reconfiguration of Fault Tolerant Algorithm when Actuator Failure of a Pixhawk based Quad-copter
Geun Hwan Kim
Korea Aerospace University
KOREA
Hot Gas Ingress Analysis with Purge Hole Design in Rotor-Stator System
Hyungyu Lee
Hanyang University
KOREA
Simulation of Separated Vortex for a Stalled Multi-Element Airfoil
Xinyu Wang
Fudan University
CHINA
Structured H∞ Control Design for the Hypersonic Experimental Aircraft Model in the Descent Trajectory Phase
Masaharu Hiruma
The Unversity of Tokyo
JAPAN
Multivariable Real-time Decoupling Control of Aviation Turbofan Engines
Dr Kai Peng
Northwestern Polytechnical University
CHINA
A Preliminary Investigation into High-Enthalpy Free-Flying Model Experiments
Christopher James
University of Queensland
AUSTRALIA
15:20 – 15:40 Flight Path Planning and Signal Behavior Analysis of a LALE Solar-powered UAV for Communication Relay
Kee-ho Yu
Chonbuk National University
KOREA
Experimental Investigation on Heat Transfer and Flow Characteristics of an Integral Internal Cooling Structure of Turbine Guide Vane
Guodong LI
Northwestern Polytechnical University
CHINA
POD-based surrogate modeling of transitional flow past rough flat plates simulated by k-ω-γ-Ar transition model
 Muchen Yang
Tsinghua University
CHINA
Prognostics and Health Management (PHM) Technology of Civil Aircraft
Xu Qinghong
 Commercial Aircraft Corporation of China
CHINA
Research on Fault Diagnosis for Secondary Power Supply and Fuel Pump Motor Based on Data Models Ensemble
Hongyu Zhu
Aviation Industry Corporation of China
CHINA
The Optimal Design of Turbine Rotor For A Micro Gas Turbine
 Mingheng Gu
Enn Energy Power Technology (shanghai) Co., Ltd (ennp)
CHINA
15:40 – 16:00 Afternoon tea
Ballroom Gallery and Garden Terrace Galley
Structures/Materials VI Unmanned Systems VI Propulsion IV Aerodynamics IV Aerospace Operations II Electric Systems Aerospace Systems Design VI
Chair: Gareth Vio Chair: Haiyin Piao Chair: Fabian Rogg Chair: Fangliang Liu Chair: Takakage Arai Chair: Jian Fu Chair: Takehiro Higuchi
16:00 – 16:20 Experimental and numerical analysis for post-buckling behavior of integral multi-spar composite box
Guofan Zhang
Aviation Industry Corporation of China
CHINA
Datalink Delay Induced UAV Payload Releasement Error Compensation Based on Forward Estimated Kalman Filter
Haiyin Piao
AVIC Shenyang Aircraft Design and Research Institute
CHINA
Thrust calibration method study during Engine power simulation
Runsheng He
Aviation Industry Corporation of China
CHINA
Preliminary investigation on vortex structures generated from the flat plate by using wake measurement
ThaiDuong Nguyen
National Defense Academy of Japan
JAPAN
The Research on Aircraft Nose Landing Gear Bay Damage
Kaijun Yin
Aviation Industry Corporation of China
CHINA
Braking Performance Analysis of No-Back Device for Electrical Trimmable Horizontal Stabilizer Actuator
Jian Fu
Beihang University
CHINA
Aerodynamic and Aero-optic Computation of a Lateral Jet-controlled High-speed Vehicle Operating at Medium Altitudes
Kwangseok Oh
Seoul National University
KOREA
16:20 – 16:40 Aero-Servo-Elasticity Capability added to KARI Aeroelasticity Analysis Software, pyFlutter
Seung-Kil Paek
Korea Aerospace Research Institute
KOREA
Transition flight mode control strategy for Quad-Tiltrotor aircraft
Kwangwoo Jang
KAIST
KOREA
Numerical Study on the Unsteady Impingement-Film Cooling Characteristics in Turbine Shroud
Jie Zhang
Northwestern Polytechnical University
CHINA
Low Speed Buffet Simulation using High-Resolution Delayed-DES with Improved LES/RANS Transition
Dr Keiichi Kitamura
Yokohama National University
JAPAN
Wake Encounter Analysis Capability added to KARI Aeroelasticity Analysis Software, pyFlutter
Dr Danbi Hong
Korea Aerospace Research Institute
KOREA
Cost Estimation Methods for Hybrid-Electric General Aviation Aircraft
D. Felix Finger
RMIT University
AUSTRALIA
Thermodynamic Performance Charateristics of The Separate type Rotary Engine Along The Design Parameters
Dockjong Ki
Tenergy Co.,Ltd
KOREA
16:40 – 17:00 Prediction for the Strength of Cylindrical Composite Lattice Structures Based on Failure Stresses from Different Test Fixtures
Min-Hyeok Jeon
Chungnam National University
KOREA
Introduction of The Ground Test Environment for DPSM (Disaster and Public Safety Multicopter)
Heemin Shin
Korea Aerospace Research Institute
KOREA
Numerical Simulation on CH4 Fueled Scramjet with Pilot Flame and Air Jet Throttling
Zhuhe Zhang
Ustc
CHINA
A Theoretical and Numerical Study of the Vibration-Excitation Effect on the Type IV Shock Interaction
Jun Peng
Chinese Academy of Science
CHINA
Research on Key Technologies of Aviation Permanent Magnet Brake
Dapeng Wang
Avic Nanjing Engineering Institute of Aircraft System
CHINA
Performance Assessment and Comparison of a Tilt Rotor UAV Using Hybrid-Electric Propulsion Systems
Yangping Deng
Northwestern Polytechnical University
CHINA
Numerical Investigation of Aerodynamic Performance for a Canard Rotor Wing Aircraft in Late Conversion Mode
Chao Pang
Northwestern Polytechnical University
CHINA
17:00 – 17:20 The Characteristics for Mode I Interlaminar Fractures of Adhesive Bonded Composite-Composite DCB Specimen
Haeri No
Chungnam National University
KOREA
Toward Machine Learning-Based Anomaly Detection for Swarm Drones
Hyojung Ahn
Kaist, Kari
KOREA
Influence of flow condition and centrifugal effect on combustion characteristics in an annular combustor
Junjie Miao
Nanjing University of Aeronautics and Astronautics
CHINA
Study on the numerical simulation of aircraft unsteady icing based on ghost cell method
Chunling Zhu
Nanjing University of Aeronautics and Astronautics
CHINA
Methodology and organizational design to realize the system integration necessary for the development of commercial aircraft
Nobuo Kishi
Churyo Engineering Co. Ltd & Osaka Prefecture University
JAPAN
Impact of Propulsion Technology Levels on the Sizing and Energy Consumption for Serial Hybrid-Electric General Aviation Aircraft
Jonas Ludowicy
RMIT University
AUSTRALIA
Development of a High Enthalpy Driver in an Expansion Tube for Generating Uranus Entry Flow Conditions
Matthew Thompson
University of Queensland
AUSTRALIA
17:20 – 17:40 Structure Safety Analysis of Composite Lattice Structure with Inspection Window
Dong Geon Kim
Hankuk Fiber Co.,ltd
KOREA
Study on Laser Guidance System for UAV Take-Off
Yasuo Obikane
Hue Industrial College
JAPAN
Flow characteristics and particle deposition of cooling channels of different shapes of staggered turbulent flow columns
Xiaoyu Shi
Northwestern Polytechnical University
CHINA
Numerical Simulation of High-Lift Airfoils at Low Speed Based on Overset Grid
Yiming Du
Northwestern Polytechnical University
CHINA
Research on Digital Standard Form and Model of Aviation Manufacturing Industry
Jianghui Zeng
China Aero-polytechnology Establishment
CHINA
Effect of bleeding air for aircraft auxiliary power unit on combustor flow characteristics
Weidong Huang
Nanjing Engineering Institute of Aircraft Systems
CHINA
17:40 – 18:00 Structural Analysis of a curved fiber Composite Fan Blade
GuoHong Chen
Beihang University
CHINA
Low-Aspect-Ratio Wing Aerodynamics at Low Reynolds Numbers using Active Turbulence Grid with Hybrid Operation
Makoto Mizoguchi
National Defense Academy
JAPAN
Unsteady and Stochastic Behavior of Kerosene Concentration in Crossflow
Yongsheng Zhao
China Academy of Aerospace Aerodynamics
CHINA
An Experimental study of skin friction reduction in a Turbulent Boundary Layer by Micro Blowing
 Jie Zheng
Northwestern Polytechnical University
CHINA
UAF Modelling of Urban Air Mobility Operation
Yan Cai
Aviation Industry Development Research Center of China
CHINA
Sensitivity Analysis of General Aviation Aircraft with Parallel Hybrid-Electric Propulsion Systems
René Rings
RMIT University
AUSTRALIA
Flight Control of Asymmetric Variable-Span Morphing Aircraft Using Nonlinear Dynamic Inversion
Jihoon Lee
Seoul National University
KOREA
19:00 – 22:00 APISAT Conference Dinner
Seaworld Gold Coast