Forum Schedule

Conference Activities

1. September 8, 2013: Visiting Helicopter Exposition and AVIC Helicopter.

2. September 9, 2013: Opening Ceremony and Keynote Speeches. 40 minutes presentation and 10 minutes Q&A for every keynote speech.

3. September 10, 2013 and Morning, September 11, 2013: Session Speeches. 20 minutes presentation and 5 minutes Q&A for every session speech.

4. Afternoon, September 11, 2013: Visiting Airbus and Industries Tianjin.

5. September 12, 2013, Leave Conference Hotel


Note:

1. The conference schedule will be put on the website of the ARF soon.

2. A common PC in every meeting room will be provided to show your presentation.

3. Your presentation ppt file will be copied into the common PC at the registration desk in Grand Skylight Hotel lobby.



Conference Schedule

Sunday, September 8, 2013

Visiting Helicopter Exposition and AVIC Helicopter

Monday, September 9, 2013

9:00~9:30

Opening Ceremony

Conference Room , 2nd Floor, Grand Skylight Hotel

9:30~17:15

Keynote Presentations

9:30~10:15

K1

The Future of Vertical Flight

Mr. Mike Hirschberg

Executive Director of AHS International, USA

10:15~10:30

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:30~11:15

K2

Thinking of Technological Development for Chinese Helicopter

Mr. Ximin Wu

Chief Engineer of China Helicopter Design and Research Institute, China

11:15~12:05

K3

Research Highlights and Educational Activities at the Penn State Vertical Lift Research Center

Prof. Edward Smith

Director of Vertical Lift Research Center of Excellence, Department of Aerospace Engineering, Penn State University, USA

12:05~13:05

Buffet, 1st floor Grand Skylight Hotel

14:00~14:45

K4

A Glimpse into the Next 20 Years of Vertical Flight

Dr. James Wang

Vice President of Research and Technology

Agusta-Westland Company, Italy

14:45~15:30

K5

A Unified Approach for Reduced-Order

Modeling of Rotor Blades

Prof. Dewey H Hodges

School of Aerospace Engineering, Georgia Institute of Technology, USA

15:30~15:45

Coffee Break, 2nd Floor, Grand Skylight Hotel

15:45~16:30

K6

Overview of High-Advance Ratio Aeromechanics of a Slowed Rotor

Alfred Gessow Prof. Inderjit Chopra

Director of Afred Gessow Rotorcraft Center

Department of Aerospace Engineering

University of Maryland, USA

16:30~17:15

K7

Numerical Study of Shipborne Rotors

Professor George N. Barakos

AWLARC Academic Director School of Engineering

The University of Liverpool, UK

18:30~20:30

Banquet and Awards

Tuesday, September 10, 2013

Session 1 Presentations: Aerodynamics

Meeting Room 1, 2nd Floor, Grand Skylight Hotel

9:00~9:25

S1R1N01

Assessment of BVI Noise Reduction by an Active Tab through Numerical Simulations

Hideaki Sugawara,

Engineering Solution Division

Ryoyu Systems Co., Ltd

Ryoko South Bldg, Japan

9:25~9:50

S1R1N02

Active Flow Control on Separation and Post-Stall of Rotor Airfoil by Using Synthetic Jet and Parametric Analyses

Zhao Guo-Qing, Zhao Qi-Jun

Lab. of Rotorcraft Aeromechanics

Nanjing University of Aeronautics and Astronautics, China

9:50~10:15

S1R1N03

Derivation of Convective Kirchhoff’s Formula for Far-field Propagation of Sound

Yong Woo Lee and Duck Joo Lee

Division of Aerospace Engineering

School of Mechanical Aerospace & Systems Engineering

KAIST, Korea

10:15~10:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:35~11:00

S1R1N04

The analysis of the influence of Rotor Anti-Torque System’s Structure Parameters to Its Aerodynamic Characteristics

Tang Min, Tang Zheng-fei and Wu Hao-dong

Lab. of Rotorcraft Aeromechanics

Nanjing University of Aeronautics and Astronautics, China

11:00~11:25

S1R1N05

Prediction of Fuselage Surface Pressure in Rotor-Fuselage Interactions Using an Integral Formulation of Poisson Equation

Ji Sung Jang

Dynamics Research Department

Advanced Technology Institute

Hyundai Heavy Industries

       Se Hwan Park and Duck Joo Lee

Aeroacoustics Laboratory, Division of Aerospace Engineering

School of Mechanical, Aerospace and Systems Engineering, KAIST, Korea

11:25~11:50

S1R1N06

Aerodynamic Shape Optimization of Rotor Airfoil Using a Viscous Continuous Adjoint Method

Wu Qi, Zhao Qi-Jun and Wang Qing

Lab. of Rotorcraft Aeromechanics

Nanjing University of Aeronautics and Astronautics, China

12:00~13:00

Buffet, 1st floor Grand Skylight Hotel

14:00~14:25

S1R1N07

PIV Test Investigation of Hovering Rotor Tip Vortex and Free Vortex Wake Simulation

Wu Jie, Yang Yong-dong and Huang Ming-qi

China Aerodynamics Research and Development Center, Mianyang, China

14:25~14:50

S1R1N08

BVI Noise Control Through Feedback Based on Pressure Signals on Blade

Yasutada Tanabe

Rotary Aircraft Section

Aircraft Systems Research Group

Japan Aerospace Exploration Agency, Japan

14:50~15:15

S1R1N09

Detailed Aerodynamic Analysis of Ducted Tail Rotor Using an Structured Moving-embedded Grid and Multi-grid Method

Ni Tong-Bing and Zhao Qi-Jun

Lab. of Rotorcraft Aeromechanics

Nanjing University of Aeronautics and Astronautics, China

15:15~15:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

15:35~16:00

S1R1N10

Design, Performance Evaluation and Contribution of Each Component of Ducted Fan UAV in Hover

Minjun Park, Division of Aerospace Engineering, KAIST, Daejeon, Korea

Jisung Jang, Dynamics Research Department, Advanced Technology Institute, HYUNDAI Heavy Industries, Ulsan, Korea

Duck-Joo Lee, Division of Aerospace Engineering, KAIST, Daejeon, Korea

16:00~16:25

S1R1N11

Analysis on Aerodynamic and Acoustic Characteristics for Scissors Tail-Rotors in Forward Flight

Fan Feng, Shi Yong-Jie and Xu Guo-Hua

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

16:25~16:50

S1R1N12

Implementation of Adaptive Wavelet Method for Hovering Rotor Aerodynamic Analysis

Sanghyun Chae, Sejong Oh and Kwanjung Yee

Department of Aerospace Engineering

Pusan National University, Korea

16:50~17:15

S1R1N13

An Improved Dynamic Stall Model for Rotor Airfoil Based on Experimental Investigations

Wang Qing, Zhao Qi-jun and Zhao Guo-qing

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

18:00~19:30

Buffet, 1st floor Grand Skylight Hotel

20:00~22:00

Visiting Seaport of Tianjing

Session 2 Presentations: Dynamics

Meeting Room 2, 2nd Floor, Grand Skylight Hotel

9:00~9:25

S2R2N01

Active Control of Electrically Controlled Rotor for Both Primary Control and Active Vibration Reduction

Ma Jinchao, Lu yang

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

9:25~9:50

S2R2N02

Dynamic Characteristic Study of Hingeless Blade Stiffness Reinforcement for Bearingless Rotor Whirl Tower Test

Taejoo Kim, Chulyong Yun, Youngjoong Kee and Seung-ho Kim

Rotor Department

Rotorcraft Technology Division

Korea Aerospace Research Institute, Korea

Sungnam Jung

Department of Aerospace Information Engineering

Konkuk University, Korea

9:50~10:15

S2R2N03

An Active Fuzzy Control for Vibration Reduction of a Smart Rotor with Trailing-edge Flaps

Yamin Wang

China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

10:15~10:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:35~11:00

S2R2N04

Analysis of Dynamic Characteristics of Asymmetric Bifilar Pendulum Absorber

Si Ying-zhan, Gao Ya-dong and Wang Hua-ming

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

11:00~11:25

S2R2N05

Corotational Formulation for Nonlinear Static and Dynamic Analysis of Thin Shells with Finite Rotation

Yang Jinsong and Xia Pinqi

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

11:25~11:50

S2R2N06

Dynamics of Helicopter Main Rotor Bifilar Vibration Absorber with Epicycloid Path

Jun Zhao and Mingzhong Wu

China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

12:00~13:00

Buffet, 1st floor Grand Skylight Hotel

14:00~14:25

S2R2N07

Controlled Parameters Optimization and Active Control of Helicopter Vibration by Using Piezoelectric Stack Actuators

Laishou Song, De Meng and Pinqi Xia

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

14:25~14:50

S2R2N08

Trim Analysis of a Bearingless Rotor based on Improved Flexible Multi-body Dynamics

Wonjong Eun, Haeseong Cho, Hanyeol Ryu and SangJoon Shin

School of Mechanical and Aerospace Engineering

Seoul National University, Korea

YoungJung Kee

Korea Aerospace Research Institute, Korea

14:50~15:15

S2R2N09

Modal Measurement of Gimbaled Tilt Rotor with Advanced Geometry Blades

Linghua Dong, Weidong Yang and Peng Hou

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

15:15~15:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

15:35~16:00

S2R2N10

Influence of Aeroelastically Tailored Wing Extensions and Winglets on Whirl Flutter Stability

Jianhua Zhang and Edward Smith

Vertical Lift Research Center of Excellence, The Pennsylvania State University, USA

16:00~16:25

S2R2N11

Fluidlastic Absorbers for Lagwise Loads Reduction of Rotor Blades

Dong Han

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

Edward C. Smith

Vertical Lift Research Center of Excellence, The Pennsylvania State University, USA

16:25~16:50

S2R2N12

Dynamic Analysis and Model Identification of an Unmanned Helicopter

Guanlin Wang, Hongli Chen, Song Han and Yu Yan

Institute of Unmanned Aerial Systems Engineering

China Aerospace Science and Technology

Beijing, China

16:50~17:15

S2R2N13

Study on helicopter dynamic components life prediction technology of individual aircraft based on flight state recognition

Xinmin Li1, 2, Benyin Zeng2, Xiaoqiang Jin2 and Shenfang Yuan1

1 College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, China

2 China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

18:00~19:30

Buffet, 1st floor Grand Skylight Hotel

20:00~22:00

Visiting Seaport of Tianjing

Session 3 Presentations: Design and Flight Control

Meeting Room 3, 2nd Floor, Grand Skylight Hotel

9:00~9:25

S3R3N01

Algorithm Design of a Distributed Strap-down Inertial Navigation System for Unmanned Rotorcraft

Jiandong Guo and Yanguo Song

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

9:25~9:50

S3R3N02

Fourteen Years of Autonomous Rotorcraft Research at the Georgia Institute of Technology

Eric N. Johnson, John G. Mooney and Henrik Christophersen

Unmanned Aerial Vehicle Research Facility

School of Aerospace Engineering

Georgia Institute of Technology, USA

9:50~10:15

S3R3N03

Influence of Rotor’s Position on the Stability of a Coaxial Helicopter

Wang Qiang, Chen Ming and Song Yang

School of Aeronautic Science and Engineering, Beihang University, Beijing, China

10:15~10:30

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:30~10:55

S3R3N04

Identification Method for Constructing Helicopter Flight Dynamics Model with Rotor Degrees of Freedom

Wu Wei and Chen Renliang

Lab. of Rotor Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

10:55~11:20

S3R3N05

Longitudinal Slung-Load Guidance for Autonomous Rotorcraft Using Rapidly-Exploring Random Trees

       Eric N. Johnson and John G. Mooney

Unmanned Aerial Vehicle Research Facility

School of Aerospace Engineering

Georgia Institute of Technology, USA

11:20~11:45

S3R3N06

Flexure Section Optimization Using Advanced Particle Swarm-Assisted Genetic Algorithm

Manoj Kumar Dhadwal, Sung Nam Jung and Chang Joo Kim

       Department of Aerospace Information Engineering

Konkuk University, Korea

Tae Joo Kim

Rotor Department, Rotorcraft Program Office

Korea Aerospace Research Institute, Korea

11:45~12:10

S3R3N07

The Flight Control System of FanWing UAV Design and Simulation

Du Siliang and Tang Zhengfei

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

12:00~13:00

Buffet, 1st floor Grand Skylight Hotel

14:00~14:25

S3R3N08

The Key Facts of Establishing NH90 NFH Shipboard Operational Limitations

Lieutenant Alrik Hoencamp1, Marilena D. Pavel2 and Douwe Stapersma1

1Experimental Flight Test Engineer

Netherlands Defense Academy

2Delft University of Technology, Netherlands

14:25~14:50

S3R3N09

Nonlinear Control of Twin Helicopter with Slung Load

Yanguo Song and Huanjin Wang

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

14:50~15:15

S3R3N10

Analysis of Causes and Countermeasures of Helicopter Accident from the Engineering Viewpoint

Myeang-Hyen Bae

Research Associate, Division of Aerospace Engineering, KAIST, Korea

Yeon-Bok Chu and Duck-Joo Lee

Division of Aerospace Engineering, KAIST, Korea

15:15~15:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

15:35~16:00

S3R3N11

Morphing Airfoil Technology with Rotorcraft Applications

Lakshmi N. Sankar, Yung H. Yu

School of Aerospace Engineering, Georgia Institute of Technology, USA

Byung Yung Min

United Technologies Research Center, USA

Chee Tung (Retired)

US Army Aeroflightdynamics Directorate, NASA Ames Research Center, USA

16:00~16:25

S3R3N12

The Effects of Cyclic Pitch Control on the Aerodynamic Characteristics of Main Rotors for ABC Helicopters

Lu Weiliang  and Xu Guo-Hua

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

16:25~16:50

S3R3N13

Forward Flight Simulation of Composite Rotor Blades with Matrix Cracking and Uncertainties

Babruvahan P. Ronge and Prashant M. Pawar

SVERI’s College of Engineering, Pandharpur, India

16:50~17:15

S3R3N14

Design and Aeroelastic Stability Test of Five-Blades Froude Scaled Model Rotor

Heping Hu, Yun Zhou and Wei Meng

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

18:00~19:30

Buffet, 1st floor Grand Skylight Hotel

20:00~22:00

Visiting Seaport of Tianjing

Wednesday, September 11, 2013

Session 4 Presentations: Aerodynamics

Meeting Room 1, 2nd Floor, Grand Skylight Hotel

9:00~9:25

S4R1N01

Experimental and Numerical Investigations for Aerodynamic and Noise Characteristics of the Rotor with Improved CLOR Blade-Tip

Zhao Qi-Jun, Wang Bo, Xu Guo-Hua and Zhu Zheng

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

9:25~9:50

S4R1N02

Investigation of vorticity confinement techniques for rotorcraft wake simulation

M. Costes, R. Boisard, T. Renaud, F. Richez,

B. Rodriguez and G. Reboul

ONERA, The French Aerospace Lab

 France

9:50~10:15

S4R1N03

Analysis the different rotational velocity impact on eccentric vortex inside of the Fanwing

Wu Hao-dong, Tang Zheng-fei and Tang Min

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

10:15~10:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:35~11:00

S4R1N04

Parametric Effect Investigation on Aerodynamic Interaction Characteristics for Tandem Rotors in Forward Flight

Huang Shuilin1, Xu Guohua2, Lin Yongfeng1, Huang Jianping1, Liu Zhangwen1

1 China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

2 Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

11:00~11:25

S4R1N05

Study on Performance Enhancement of Electrically Controlled Rotor Based on 2/rev Flap Input

Wang Chao, Lu Yang, Chen Renliang

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

11:25~11:50

S4R1N06

Experimental Investigations on the Tip Vortex Trajectory and Core for Helicopter Rotors

Lin Yongfeng1, Huang Shuilin1, Zhao Qinjun2, Deng Jinghui1

1 China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

2 Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

12:00~13:00

Buffet, 1st floor Grand Skylight Hotel

14:00~17:00

Visiting Airbus and Industries Tianjin

18:30~19:30

Buffet, 1st floor Grand Skylight Hotel

Session 5 Presentations: Ice Accretion

Meeting Room 2, 2nd Floor, Grand Skylight Hotel

9:00~9:25

S5R2N01

Thermodynamic Model of Ice Accretion on Rotor Blades Considering of the Centrifugal Force

       Chen Xi and Zhao Qi-Jun

       Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

9:25~9:50

S5R2N02

Enhancement of Ultrasonic De-icing via Transient Excitation

Nicola DiPlacido, Jared Soltis and Edward Smith

Vertical Lift Research Center of Excellence, The Pennsylvania State University, USA

9:50~10:15

S5R2N03

Helicopter Rotor Performance Loss Prediction For Ice Accretion

Zhang Wei and Pan Xiying

China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

10:15~10:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:35~11:00

S5R2N04

Numerical Simulation of Airfoil Ice Accretion Phenomena

Jeewoong Kim, Lakshmi N. Sankar

School of Aerospace Engineering, Georgia Institute of Technology Atlanta USA

Christine M. Brown, Robert F. Kunz, Jules W. Lindau, Michael P. Kinzel

Department of Aerospace Engineering and Applied Research Laboratory

The Pennsylvania State University

Richard E. Kreeger

NASA Glenn Research Center, USA

11:00~11:25

S5R2N05

Study on the Numerical Simulation of Helicopter Nacelle Ventilation Cooling System

Wang Xianwei, Kuang Chuanshu and Yu jing

China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

11:25~11:50

S5R2N06

The Integration Modeling Simulation Methodology for Birdstrike Impact Prediction on Helicopter Composite Material Structures

Lü Lefeng1, , Wu Wenke1 and Sun Jinbo2

1 China Helicopter Research and Development Institute, AVICopter, Jing Dezhen, China

2 Shen Yang Aircraft Airworthiness Certification Center, CAAC, China

12:10~13:10

Buffet, 1st floor Grand Skylight Hotel

14:00~17:00

Visiting Airbus and Industries Tianjin

18:00~19:30

Buffet, 1st floor Grand Skylight Hotel

Session 6 Presentations: CFD/CSD

Meeting Room 3, 2nd Floor, Grand Skylight Hotel

9:00~9:25

S6R3N01

Analysis of Rotor Airloads Based on CFD/CA Loose Coupling

Xiao Yu, Xu Guo-Hua and Shi Yong-Jie

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

9:25~9:50

S6R3N02

Evaluation of a Hybrid Method of CFD and Prescribed Wake Model for Rotary Wings in Hover

Shigeru Takeda 1, Hideaki Sugawara 3 , Masahiko Sugiura 2 , Masahiro Kanazaki 1 , Yasutada Tanabe 2, Masatoshi Harigae 1

1 Tokyo Metropolitan University, Japan

2 Institute of Aeronautical Technology, Japan Aerospace Expolaration Agency, Japan

3 East Japan Engineering Group, Ryoyu Systems Co., Ltd., Nagoya, Aichi, Japan

9:50~10:15

S6R3N03

Aeroelastic Characteristics Analysis of Helicopter Rotors Based on CFD/CSD Coupling Method

Wang Junyi, Zhao Qijun and Xiao Yu

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

10:15~10:35

Coffee Break, 2nd Floor, Grand Skylight Hotel

10:35~11:00

S6R3N04

Improvements to the Hybrid Method of CFD and Prescribed Wake Model for Rotorcraft Aeroacoustics and Aerodynamics Prediction

Masahiko Sugiura and Yasutada Tanabe

Aircraft Systems Research Group

Institute of Aeronautical Technology

Japan Aerospace Exploration Agency, Japan

Hideaki Sugawara

Engineering Solution Division

East Japan Engineering Group, Ryoyu Systems Co., Ltd., Nagoya, Aichi, Japan

11:00~11:25

S6R3N05

Research on Circulation Controlled Tail Boom with Irregular Slots Using CFD

Chen Chen, Gao Ya-dong and Wang Hua-ming

Lab. of Rotorcraft Aeromechanics

College of Aerospace Engineering

Nanjing University of Aeronautics and Astronautics, China

11:25~11:50

S6R3N06

The Research of The Flow Over a Rotor Using Overset-Grid Method

Niu Song, Zhang Wei and Cao pusun

China Helicopter Research and Development Institute, AVICopter, Jingdezhen, China

12:00~13:00

Buffet, 1st floor Grand Skylight Hotel

14:00~17:00

Visiting Airbus and Industries Tianjin

18:00~19:30

Buffet, 1st floor Grand Skylight Hotel

ThursdaySeptember 12, 2013, Leave Hotel