Asian-Australian Rotorcraft Forum 2013 Paper List

ARF welcome by AVICThank you for participating in the 2nd Asian-Australian Rotorcraft Forum (ARF) / 4th International Basic Research Conference on Rotorcraft Technology (IBRCRT) on September 9-11, in Tianjin, China.

All conference attendees are allowed to download the papers in pdf format at no cost. Please click on the links below to save each paper.

Those who did not attend the conference may purchase the papers or a CD-ROM of all the papers through the AHS Online Store. 

Photos from the event are available at https://vtol.org/qr/tianjin-2013.


Front Matter and Table of Contents

Active Control of Electrically Controlled Rotor for Both Primary Control and Active Vibration Reduction
Ma Jinchao and Lu yang, Nanjing University of Aeronautics and Astronautics

Active Flow Control on Separation and Post-Stall of Rotor Airfoil by Using Synthetic Jet and Parametric Analyses
Zhao Guo-Qing, Zhao Qi-Jun, Nanjing University of Aeronautics and Astronautics

Aerodynamic Shape Optimization of Rotor Airfoil Using a Viscous Continuous Adjoint Method
Wu Qi, Zhao Qi-Jun, Wang Qing, Nanjing University of Aeronautics and Astronautics

Aeroelastic Characteristics Analysis of Helicopter Rotors Based on CFD/CSD Coupling Method
Wang Junyi, Zhao Qijun, Xiao Yu, Nanjing University of Aeronautics and Astronautics

Algorithm Design of a Distributed Strap-down Inertial Navigation System for Unmanned Rotorcraft
Jiandong Guo, Yanguo Song, Nanjing University of Aeronautics and Astronautics

An Active Fuzzy Control for Vibration Reduction of a Smart Rotor with Trailing-edge Flap
Yamin Wang, China Helicopter Research and Development Institute

An Improved Dynamic Stall Model for Rotor Airfoil Based on Experimental Investigations
Wang Qing, Zhao Qi-jun, Zhao Guo-qing, Nanjing University of Aeronautics and Astronautics

Analysis of Causes and Countermeasures of Helicopter Accident from the Engineering Viewpoint
Myeang-Hyen Bae, Yeon-Bok Chu, Duck-Joo Lee, KAIST

Analysis of Dynamic Characteristics of Asymmetric Bifilar Pendulum Absorber
SI Ying-zhan, GAO Ya-dong, WANG Hua-ming, Nanjing University of Aeronautics & Astronautics

Analysis of Rotor Airloads Based on CFD/CA Loose Coupling
Xiao Yu, Xu Guo-Hua, Shi Yong-Jie, Nanjing University of Aeronautics and Astronautics

Analysis on Aerodynamic and Acoustic Characteristics for Scissors Tail-Rotors in Forward Flight
Fan Feng, Shi Yong-Jie, Xu Guo-Hua, Ye Zhou, Nanjing University of Aeronautics and Astronautics

Analysis The Different Rotational Velocity Impact On Eccentric Vortex Inside Of The Fanwing
Wu Hao-dong, Tang Zheng-fei, Tang Min, Science and Technology on Rotorcraft Aeromechanics Laboratory

Assessment of BVI Noise Reduction by an Active Tab through Numerical Simulations
Hideaki Sugawara Research Engineer, Ryoyu Systems Co., Ltd.

BVI Noise Control Through Feedback Based on Pressure Signals on Blade
Yasutada Tanabe, Japan Aerospace Exploration Agency; Hideaki Sugawara, Ryoyu Systems Co., Ltd.

CFD Calculations on the Unsteady Aerodynamic Force of Tiltrotor in Conversion Mode
Li Peng, Zhao Qi-Jun, Nanjing University of Aeronautics and Astronautics

Controlled Parameters Optimization and Active Control of Helicopter Vibration by Using Piezoelectric Stack Actuators
Laishou Song, De Meng, Pinqi Xia, Nanjing University of Aeronautics and Astronautics

Corotational Formulation for Nonlinear Static and Dynamic Analysis of Thin Shells with Finite Rotation
Yang Jinsong, Xia Pinqi, Nanjing University of Aeronautics and Astronautics

Derivation Of Convective Kirchhoff’s Formula For Far-Field Propagation Of Sound
Yong Woo Lee, Duck Joo Lee, School of Mechanical Aerospace & Systems Engineering

Design and Aeroelastic Stability Test of Five-Blades Froude Scaled Model Rotor
Heping Hu, Yun Zhou, Wei Meng, CHRDI

Design, Performance Evaluation And Contribution Of Each Component Of Ducted Fan UAV In Hover
Minjun Park, KAIST; Jisung Jang, HYUNDAI Heavy Industries; Duck-Joo Lee, KAIST

Detailed Aerodynamic Analysis of Ducted Tail Rotor Using an Structured Moving-embedded Grid and Multi-grid Method
Ni Tong-Bing, Zhao Qi-Jun, Nanjing University of Aeronautics and Astronautics

Dynamic Analysis and Model Identification of an Unmanned Helicopter
Guanlin Wang, Hongli Chen, Song Han, and Yu Yan, Institute of Unmanned Aerial Systems Engineering

Dynamic Characteristic Study of Hingeless Blade Stiffness Reinforcement for Bearingless Rotor Whirl Tower Test
Taejoo Kim, Chulyong Yun, Youngjoong Kee, and Seung-ho Kim, Korea Aerospace Research Institute; Sungnam Jung, Konkuk University

Enhancement of Ultrasonic De-icing via Transient Excitation
Nicola DiPlacido, Jared Soltis, Edward Smith, and Jose Palacios, The Pennsylvania State University

Evaluation of a Hybrid Method of CFD and Prescribed Wake Model for Rotary Wings in Hover
Shigeru Takeda, Tokyo Metropolitan University; Masahiko Sugiura, Yasutada Tanabe, Japan Aerospace Exploration Agency; Hideaki Sugawara, Ryoyu Systems Co., Ltd; Masahiro Kanazaki and Masatoshi Harigae, Tokyo Metropolitan University

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, Zhu Zheng, Nanjing University of Aeronautics and Astronautics

Experimental Investigations on Tip Vortex Trajectory and Core for Helicopter Rotors
Yongfeng Lin, Shuilin Huang, JingHui Deng, CHRDI; Qijun Zhao, NUAA

Flexure Section Optimization Using Advanced Particle Swarm-Assisted Genetic Algorithm
Manoj Kumar Dhadwal, Sung Nam Jung, Chang Joo Kim, Konkuk University; Tae Joo Kim, Korea Aerospace Research Institute

Flow Field Simulation of Rotor in Ground Effect for Steady and Transition Flight with Low Forward Speed
Chen Ren-liang, Xin Ji, Li Pan, Nanjing University of Aeronautics and Astronautics

Fluidlastic Absorbers for Lagwise Loads Reduction of Rotor Blades
Dong Han, Nanjing University of Aeronautics and Astronautics; Edward C. Smith, The Pennsylvania State University

Forward Flight Simulation of Composite Rotor Blades with Matrix Cracking and Uncertainties
Dr. Babruvahan P. Ronge, Dr. Prashant M. Pawar, SVERI’s College of Engineering

Fourteen Years of Autonomous Rotorcraft Research at the Georgia Institute of Technology
Eric N. Johnson, Henrik Christophersen, John G. Mooney, Georgia Institute of Technology

Helicopter Dynamic Components Life Prediction of Individual Aircraft Based on Flight State Recognition
Xinmin Li, Benyin Zeng, Xiaoqiang Jin, China Helicopter Research and Development Institute; Shenfang Yuan, Nanjing University of Aeronautics and Astronautics

Helicopter Rotor Performance Loss Prediction For Ice Accretion
Zhang Wei, Pan Xiying, AVIC Helicopter Research & Development Institute

Identification Method for Constructing Helicopter Flight Dynamics Model with Rotor Degrees of Freedom
Wu Wei, Chen Renliang, Nanjing University of Aeronautics and Astronautics

Implementation of Adaptive Wavelet Method for Hovering Rotor Aerodynamic Analysis
Sanghyun Chae, Sejong Oh, Kwanjung Yee, Pusan National University

Improvements to the Hybrid Method of CFD and Prescribed Wake Model for Rotorcraft Aeroacoustics and Aerodynamics Prediction
Masahiko Sugiura, Yasutada Tanabe, Japan Aerospace Exploration Agency; Hideaki Sugawara, Ryoyu Systems Co., Ltd.

Influence of Aeroelastically Tailored Wing Extensions and Winglets on Whirl Flutter Stability
Jianhua Zhang, Edward C. Smith, The Pennsylvania State University

Influence of Rotor’s Position on the Stability of a Coaxial Helicopter
Wang Qiang, Chen Ming, Song Yang, Beihang University

Integrated Analyses about Aerodynamic and Stealth Characteristics of Airfoil Based on CFD/CEM Coupling Method
Jiang Xiang-wen, Zhao Qi-Jun, Zhao Guo-Qing, Nanjing University of Aeronautics and Astronautics

Investigation Of Vorticity Confinement Techniques For Rotorcraft Wake Simulation
M. Costes, R. Boisard, T. Renaud, F. Richez, B. Rodriguez, and G. Reboul, ONERA

Investigation on the Flow Field over a Rotor using Overset-grid Method
Niu Song, Zhang Wei, Cao Pusun, AVIC Helicopter Research & Development Institute

Keynote: A Unified Approach for Reduced-Order Modeling of Rotor Blades
Dewey H. Hodges, Prof., Georgia Institute of Technology

Keynote: The Future of Vertical Flight
Mike Hirschberg, AHS Executive Director

Longitudinal Slung-Load Guidance for Autonomous Rotorcraft Using Rapidly-Exploring Random Trees
Eric N. Johnson and John G. Mooney, Georgia Institute of Technology

Modal Measurement of Gimbaled Tilt Rotor with Advanced Geometry Blades
Linghua Dong, Weidong Yang, Peng Hou, Nanjing University of Aeronautics and Astronautics

Modeling and Parameter Sensitivity Analysis of Helicopter Main Rotor Bifilar Vibration Absorber
Jun Zhao, Mingzhong Wu, China Helicopter Research and Development Institute

Morphing Airfoil Technology with Rotorcraft Applications
Lakshmi N. Sankar, Yung H. Yu, Georgia Institute of Technology; Byung Yung Min, United Technologies Research Center; Chee Tung, NASA Ames Research Center

Nonlinear Control of Twin Helicopter with Slung Load
Yanguo Song, Huanjin Wang, Nanjing University of Aeronautics and Astronautics

Numerical Simulation of Airfoil Ice Accretion Phenomena
Jeewoong Kim, Georgia Institute of Technology; Christine M. Brown, The Pennsylvania State University; Richard E. Kreeger, NASA Glenn Research Center; Lakshmi N. Sankar, Georgia Institute of Technology; Robert F. Kunz, Jules W. Lindau, and Michael P. Kinzel, The Pennsylvania State University

Numerical Study Of Shipborne Rotors
G.N. Barakos, C. Crozon, R. Steij, University of Liverpool

Parametric Effect Investigation on Aerodynamic Interaction Characteristics for Tandem Rotors in Forward Flight
Huang Shuilin, CHRDI; Xu Guohua, NUAA; Lin Yongfeng, Huang Jianping, and Liu Zhangwen, CHRDI

PIV Test Investigation of Hovering Rotor Tip Vortex and Free Vortex Wake Simulation
WU Jie, YANG Yong-dong, HUANG Ming-qi, China Aerodynamics Research and Development Center

Prediction of Fuselage Surface Pressure in Rotor-Fuselage Interactions Using an Integral Formulation of Poisson Equation
Ji Sung Jang, Hyundai Heavy Industries; Se Hwan Park, Duck Joo Lee, KAIST

Research on Circulation Controlled Tail Boom with Irregular Slots Using CFD
CHEN chen, GAO Ya-dong, WANG Hua-ming, Nanjing University of Aeronautics & Astronautics

Study on a New Anti-Torque System of Rotor
Tang Zheng-fei, Feng Chen

Study on Performance Enhancement of Electrically Controlled Rotor Based on 2/rev Flap Input
Wang Chao, Lu Yang, Chen Renliang, Nanjing University of Aeronautics and Astronautics

The Effects of Cyclic Pitch Control on the Aerodynamic Characteristics of Main Rotors for ABC Helicopters
Lu Weiliang, Xu Guo-Hua, Nanjing University of Aeronautics and Astronautics

The Flight Control System of FanWing UAV Design and Simulation
Du Siliang, Tang Zhengfei, NUAA

The Integration Modeling Simulation Methodology for Birdstrike Impact Prediction on Helicopter Composite Material Structures
Lü Lefeng, Wu Wenke, AVIC Helicopter Research and Development Institute; Sun Jinbo, Shen Yang Aircraft Airworthiness Certification Center of CAAC

The Key Facts of Establishing NH90 NFH Shipboard Operational Limitations
Lieutenant Alrik Hoencamp, Netherlands Defense Academy; Marilena D. Pavel, Delft University of Technology; Douwe Stapersma, Netherlands Defense Academy

Thermodynamic Model of Ice Accretion on Rotor Blades Considering of the Centrifugal Force
Chen Xi, Zhao Qi-Jun, Nanjing University of Aeronautics and Astronautics

ToC: Basic Research More Advance in Rotorcraft Technology/Table of Contents
Pinqi Xia, Renliang Chen and Zhengfei Tang

Trim Analysis of a Bearingless Rotor based on Improved Flexible Multi-body Dynamics
Wonjong Eun, Haeseong Cho, Hanyeol Ryu, SangJoon Shin, Seoul National University; YoungJung Kee, Korea Aerospace Research Institute

Unmanned Helicopter Parameter Identification Based on Modified Gain Kalman Filter Algorithm
Zhang Xingwen, Chen Ming, Wang Qiang, Beijing University of Aeronautic and Astronautic