final program - arf 2019final program 8th asian/australian rotorcraft forum october 30 - november 2...

8th ASIAN / AUSTRALIAN ROTORCRAFT FORUM • ConferenCe Book4

FINAL PROGRAM

8th Asian/Australian Rotorcraft ForumOctober 30 - November 2 , 2019

Day 1 - Wednesday, October 30

08:30 Registration Open

09:30 Workshop I Workshop II

Linear Time Invariant (LTI) Models for Integrated Flight and Rotor ControlProf. Dr. J.V.R. Prasad & Assoc. Prof. Dr. Ilkay Yavrucuk

Achieving Reliable Failure Predictions in CompositesProf. Dr. Erian A. Armanios & Prof. Dr. Kemal Levend Parnas

Linear time periodic (LTP) models typical of rotorcraft dynamics are not suitable for control design since the majority of methods are based on linear models in time invariant (LTI) form. Also, handling qualities specifications are based on time invariant linear models, and thus, cannot be directly applied to the controller design using LTP models. Use of harmonic states provides a convenient framework for transformation of LTP models into LTI model approximations. The dynamic characterization using LTI models with harmonic states converges to that of the periodic system when the number of harmonic states increases. However, the increase of harmonic states produces a high dimensional model. Therefore, the size of the LTI model has to be reduced. As a consequence of this reduction several issues arise, for example, (a) sensitivity of model fidelity to the number of harmonic states employed, and (b) effect of harmonic state feedback on stability margins and handling qualities. Two important questions that need to be addressed for fidelity assessment and LTI model order reduction are: (a) what are the most appropriate fidelity metrics?, and (b) how to determine the minimal order LTI model approximation of a periodic system? In order to answer these questions, a detailed understanding of stability properties of LTP and LTI models with harmonic rotor, body and inflow states is needed. Further, integrated flight and rotor control case studies are needed in order to establish a design framework capable of simultaneously accounting for stability margins and handling qualities

Achieving quality standards needed for reliable allowables, is a standing challenge for failure predictions. To this end, an integrated approach for the diagnosis and prognosis of composites, is underscored. It encompasses: 1. Nondestructive inspection enabling 3D measurement of defect location and geometry coupled with an automated transition capability to finite element models; 2. Accurate and cost effective 3D material property measurements with a minimum number of tests and methods; and 3. Structural strength and fatigue life prognosis based upon comprehensive methods that capture the failure mechanisms associated with multiple damage modes and their interaction. Future research directions emphasize the development of composites processing simulation tools to accelerate the attainment of quality standards, high-performance hybrid material systems and high-resolution nondestructive technologies for inspection of large structures.

12:00 Lunch

13:30 Shuttle Leave from Conference Convention Center to TURKISH AEROSPACE

14:30 Technical Tour - TURKISH AEROSPACE

18:00 Welcome Reception at Conference Convention Center

8th ASIAN / AUSTRALIAN ROTORCRAFT FORUM • ConferenCe Book 5

Day 2 - Thursday, October 31

07:30 Registration

09:00 Technical Session

Main Hall Room 1 Room2 Room 3 Room 4 Room 5

Advanced Concepts 1 Aerodynamics 1 Development Programs 1 Dynamics 1 Structures 1

09:00

Performance Analysis of a Helicopter with a Variable Speed Rotor

Numerical Simulation of the Aerodynamic Interference of the Rotor/Fuselage in the transition state of the Quad-Tiltrotor UAV

Rotary wing first of class flight trials to HMS Queen Elizabeth

Power-on Effect on Longitudinal Stability in Quad Tilt Propeller Aircraft

Structural Analysis and comparison of loading capability of CNT fibre and Carbon fibre

Dong Han Du Siliang1, Zhao Qijun2, Wang Bo2

Mark Walsh1, Anthony Laurence Dyer1, Scott Mcquaid1, Natalie Taylor1, Gordon Stewart1, Harry Boden1, Adam Hare1, Steven Baldie2, Hardiman Keith1

Yebin Lee1, Seonggi Lee2, Sejong Oh1, Jaehun Choi3, Yunggyo Lee3, Taehwan Cho3, Donghun Park1

Renuka Sahu, Dineshkumar Harursampath

Department of Helicopter, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

1Jiangsu Key Laboratory of Advanced Manufacturing Technology, HuaiYin Institute of Technology, Huaian 223003, China; National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

2National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China

1QinetiQ, MoD Boscombe Down, UK

2Rotary Wing Test & Evaluation Squadron, MoD Boscombe Down, UK

1Aerospace Engineering, Pusan National University, Pusan, South Korea

2Hyundai Rotem Company, Gyeonggi-do, South Korea

3Korea Aerospace Research Institute, Daejeon, South Korea

Aerospace Engineering,Indian Institute of Science,Bangalore,India




09:30

Comparison of the AFCS in Mechanical and Fly-By-Wire FCSs

Investigation of Aerodynamic Interaction of a Lift Offset Coaxial Rotor by Numerical Simulation

Requirements Management within Model Environment

Dynamic characteristics of tilt-rotor systems on advanced high-altitude VTOL vehicle

Aeroelastic stability analysis of composite blades based on cross-section parametric modeling

Abdurrahman Yasin Yorulmaz, Mahmut Bilgin, Abdullah Vural

Kaito Hayami1, Hideaki Sugawara1, Yasutada Tanabe2, Masaharu Kameda1

Volkan Mert Xiayang Zhang, Bo Wang, Qijun Zhao, Guoqing Zhao

Li Ma, Qijun Zhao, Kai Zhang

Turkish Aerospace Industries Inc.

1Department of Mechanical Systems Engineering, Tokyo University of Agriculture and Technology, Tokyo, Japan

2Aviation Systems Research Unit, Japan Aerospace Exploration Agency, Tokyo, Japan


National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics Nanjing, Jiangsu, China

National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing,China

10:00 Coffee Break

10:30 Opening Ceremony (Main Hall)




11:30

Utilizing rapid prototyping in fabrication of rotor blade molds

Numerical Study of Air-Launched Projectiles for Fixed and Rotary Wing Aircraft Safety

Independent Development of Helicopter Flight Dynamic Models for Full Flight Simulators

A numerical methodology to predict torque balanced conditions of a tip-jet rotor

Reliability Analysis of Multi-State on Helicopter Emergency Flotation System

Özgür Tecer, Ali Cirit, Rıza Özcan

Sung Min Jo, Oh Joon Kwon Ilkay Yavrucuk1, Gönenç Gürsoy2

Daun Park, Soo Hyung Park Xing Guo, Jianhong Sun, Bin Hou, Zhi Sun


Korea Advanced Institute of Science and Technology

1 Middle East Technical University, Ankara, Turkey

2 Aerotim Engineering, Ankara, Turkey

Department of Aerospace Information Engineering, Konkuk University, Seoul, South Korea.

Key Laboratory of Aircraft environment control and life support, MIIT, Nanjing University of Aeronautics & Astronautics, Nanjing, 210016, China




12:00

The Conceptual Study of Antagonistic Shape Memory Alloy Actuator System to Morph the Blade Tip

Multi-Rotor Finite State Wake Models Based on Superposition Approaches: VPSIM and PPSIM

Flight Test Risk Calculator (RIZIKO)

Solving Rotorcraft Emergency Landing Trajectory Optimization Problems Using New Approach for Direct Method

Hasan Hüseyin Saygılı1, Halil Onat Tuğrul2, Benat Koçkar2

Feyyaz Guner, J. V. R. Prasad Ersin Kocaadam, Eril Balcıoğlu, Çağrı Çıkrıkcı, Ilker Uysal, Meriç Erdem, Arif Ateş, Gökhan Virlan

Yong Hyeon Nam, Seong Han Lee, Chang Joo Kim

1Turkish Aerospace Industries Inc.2Hacettepe University

School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, USA


Konkuk University, Seoul, Republic of Korea

12:30 Lunch

13:30 Keynote Speech Session (Main Hall)Keynote Speech Session (Main Hall) Keynote - ARF Representatives, China/Japan/India/Korea/Australia/Turkey Update of Rotorcraft R&D Activities

15:00 Coffee Break



Development Programs 2 Unmanned Systems 1 Aerodynamics 2 Rotorcraft Design 1 Dynamics 3 Structures 2

15:30

Maiden flight of T625 Gökbey Helicopter

Markovian Approach for Learning Based Flight Condition Recognition Methods

Investigation on Aerodynamic Efficiency of Multi-Ducted Fan in Forward Flight

Effect of Lift and Thrust Share on Flight Performance of a Compound Helicopter

Bell 412 System Identification and Model Fidelity Assessment for Hover and Forward Flight

Highly efficient structural optimization of wind turbine blade sections using a mixed beam approach with Bezier curves

Ersin Kocaadam, Gökhan Virlan, Arif Ateş, Çağrı Çıkrıkcı, Ilker Uysal, Meriç Erdem, Eril Balcıoğlu, Alper Kurdoğlu

Uğur Kalkan, Murat Şenipek, Arda Yücekayalı

Nahyeon Roh, Donghun Park, Sejong Oh

Kelong Yang Susanne Seher-Weiss1, Mark B. Tischler2, Pavle Scepanovic1, Arthur Gubbels3

Jae Seong Bae, Sung Nam Jung



Department of Aerospace Engineering, Pusan National University, Busan, South Korea

National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

1DLR Institute of Flight Systems, Braunschweig, Germany2Aviation Development Directorate, CCDC Aviation & Missile Center, Moffett Field, CA3NRC, Flight Research Laboratory, Ottawa, Ontario, Canada

Konkuk University



Development Programs 2 Unmanned Systems 1 Aerodynamics 2 Rotorcraft Design 1 Dynamics 3 Structures 2

16:00

Safety of flight tests for the maiden flight of prototype helicopters “T625 Gökbey case”

Logıcal Algorıthm Desıgn With State Machınery Approach For Automatıc Flıght Control System Of Helıcopter

Mechanism research on Rotor BVI Noise Reduction by Parameter Analysis of HHC Method

T625 Mathematical Model Integration for Rapid Pilot-in-the-loop Environment

Feedforward-feedback control of a strut driven by piezoelectric stack actuators

Composition of three-dimensional finite element structural analysis model based on the X-ray scanned images of HART II blades

Ersin Kocaadam, Meriç Erdem, Çağrı Çıkrıkcı, Ilker Uysal, Eril Balcıoğlu, Arif Ateş, Gökhan Virlan

Sınan Özcan, Mustafa Gürler, Şerafettin Tüzel

Siyu Chen, Bo Wang, Qijun Zhao

Emre Soranlar, Semih Yavuz, Emre Karalarlı

Laishou Song, Zhiliang Tan, Pinqi Xia

Hyun Jun Hwang, Jun Hvek Ahn, Se Hoon Chang, Sung Nam Jung



National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics Nanjing, Nanjing, China.


Aerospace Information Engineering, Engineering, Konkuk University

16:30

Flow Analysis in a Test Rig System Characterization of a Helicopter Hydraulic Power System

Design and Evaluation of Flight Control System for Unmanned Compound Rotorcraft

An Aerodynamic Study for JAXA High Speed Compound Helicopter by a Wind Tunnel Test

In-Flight Test Campaign to Validate PIO Detection and Assessment Tools

Effect of lay-up orientation and crack length propagation on fracture toughness of CFRP and GFRP laminates

Ahmet Özturan, HAsan Ali Düzağaç, Umur Afif Limon, Erhan Erbay, Alper Yasin Tiftikçi

Sung Wook Hur, Sang Ho Kang, Chang Joo Kim

Noboru Kobiki1, Yasutada Tanabe1, Hideaki Sugawara2

Michael Jones1, Marc Alexander2, Marc Höfinger1, Miles Barnett3, Perry Comeau2, Arthur Gubbels2

Burak Ogun Yavuz1, Levend Parnas2, Demirkan Coker1


Department of Aerospace Information Engineering, Konkuk University, Seoul, Republic of Korea

1JAXA2Ryoyu Systems Co., Ltd.

1Rotorcraft Department, Institute of Flight Systems, DLR, Braunschweig, Germany2Flight Research Laboratory, Ottawa, Canada3Flight Experiments, DLR, Braunschweig, Germany

1Aerospace Engineering, Middle East Technical University, Ankara, Turkey2Mechanical Engineering, TED University, Ankara, Turkey

17:00

Retrospective Analysis of Australia’s Defence Avaition Safety Framework

VFS Turkey Chapter meeting

Arvind Sinha, James Hood, Pier Marzocca

RMIT University, Australia

17:30 End of Technical Sessions

20:30 Gala Dinner


Day 3 - Friday, November 1

08:30 Registration



Aerodynamics 3 Rotorcraft Design 2 Dynamics 4 Structures 3 Unmanned Systems 2 Propulsion and Drive 1

09:00

Aerodynamic response analysis of rotor during ramp collective pitch changing by CFD method

Rotor Stall Onset Assessment Generation of Helicopter Pull-Up Maneuver with Harmony Search Optimization Method

Fatigue test of a composite structure instrumented with Fiber Bragg Grating sensors for structural health monitoring applications

Can Time-To-Contact Be Used To Model A Helicopter Autorotation?

Nonlinear Forced Response Analysis of Bladed Disks With Wedge Dampers

Kai Zhang, Qi Jun Zhao, Bo Wang, Xia Yang Zhang

Pinar Arslan Dülgar, Arda Yücekayalı, Osman Güngör, Yüksel Ortakaya

Fatih Tosun1, Uğur Kalkan1, Harun Tıraş1, Yavuz Yaman2

Cansu Karataş Demircan1, Boray Değerliyurt1, Melin Şahin2

Mushfiqul Alam, Michael Jump, Neil Cameron

H. Sefa Kizilay, Ender Cigeroglu

National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics Nanjing, Jiangsu, China


1Turkish Aerospace Industries Inc.2Aerospace Engineering Department, Middle East Technical University,Ankara,Turkey

1Turkish Aerospace Industries Inc.2Middle East Technical University

Flight Science and Technology Research Group, Department of Mechanical Materials & Aerospace Engineering, The University of Liverpool, Liverpool, United Kingdom

Middle East Technical University

09:30

Viscous Vortex Particle Method Explored for Main Rotor-Tail Rotor Interaction

Architectural composition of models by Simulink System Composer

Multibody analysis of the influence of strut-mounted vibration alleviation devices on rotor aeromechanics

2D and 3D Modelling of Delamination in Tapered Composite Laminates Using Cohesive Elements

Stability and controllability assessment of water tank release procedure from a utility helicopter in fire fighting operations

Investigating Effects of Shrouding Length on the Windage Power Losses of a Spur Gear

Arda Yucekayali, Yüksel Ortakaya

Volkan Mert Aykut Tamer, Andrea Zanoni, Matteo Daniele, Pierangelo Masarati

Saeid Hosseinpour Dashatan1, Levend Parnas2, Demirkan Coker3

Arda Çalışkan, Yıldırım Kemal Yıllıkçı, Aydın Birol Akdemir, Özge Kapulu Gülbağ

Ali Kıvanç Ersan1, Mehmet Ali Yavuz1, Murat Kadri Aktaş2



Department of Aerospace Science and Technology, Politecnico Di Milano, Milano, Italia

1Department of Mechanical Engineering, Middle East Technical University, Ankara, Turkey2Department of Mechanical Engineering, Ted University, Ankara, Turkey3Department of Aerospace Engineering, Middle East Technical University, Ankara, Turkey


1Turkish Aerospace Industries Inc.2Mechanical Engineering, TOBB ETU, Ankara, Turkey



Aerodynamics 3 Rotorcraft Design 2 Dynamics 4 Structures 3 Unmanned Systems 2 Propulsion and Drive 1

10:00

Aerodynamic Characteristics of a Quad-Rotor-Drone with Ducted Rotors

Dynamic Interface Modelling and Simulation. Part 1: Preparation and Analysis for High-Fidelity Helicopter-Ship Flight Simulations

Effects of Variable Trailing Edge Flap on Rotor Rolling Moment Characteristics

Mechanical & Material Characterization of Nomex used in Helicopter Blades

Flight Data Processing for helicopter mathematical model validation

Koichi Yonezawa1, Hironori Matsumoto2, Kazuyasu Sugiyama2, Yasutada Tanabe3, Hiroshi Tokutake4, Shigeru Sunada5

Neale Alexander Watson, Wajih Ahmed Memon, Ieuan Owen, Mark Dermot White

Guo Qing Zhao, Qi Jun Zhao, Bo Wang, Xia Yang Zhang

Khaja Moinuddin Mohmmed Shaik Bepari1, Arithra Chatterjee2, M R Bhat1, Namrata Gundiah2, Dineshkumar Harursampath1

Uğurcan Özalp

1Central Research Institute of Electric Power Company, Japan2Osaka University, Japan3Japan Aerospace Exploration Agency4Kanazawa University, Japan5Nagoya University, Japan

University of Liverpool, Liverpool, United Kingdom

National Key Laboratory of Rotorcraft Aeromechanics, College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, China

1Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India2Department of Mechanical Engineering, Indian Institute of Science, Bangalore, India


10:30 Coffee Break



Rotorcraft Design 3 Advanced Concepts 2 Unmanned Systems 3 Aerodynamics 4 Aerodynamics 5

11:00

Student Poster Session (Undergraduate and Graduate Level Students Thesis or Competition Teams Posters)

Student Poster’s Visit (Multiple Student Posters will be demonstrated in Exhibition Hall)

Dynamic Interface Modelling and Simulation. Part 2: Developing Robust Fidelity Requirements for Maritime Rotorcraft Flight Simulators

Preliminary Study on Innovative Loop Propellers for Quiet eVTOLs

Feed Forward Decoupling Controller Design for a Helicopter

Effect of Lift Share Ratio on the Aerodynamic Performance of a Winged Compound Helicopter

Multi-objective optimization design for rotor airfoil under unsteady conditions

Wajih Ahmed Memon, Neale Alexander Watson, Mark Dermot White, Ieuan Owen

Eiji Shima, Seiji Tsutsumi, Keiichiro Fujimoto

Ayşe Ilden Bayrak, Ismail Hakkı Şahin

Hideaki Sugawara1, Yasutada Tanabe2, Masaharu Kameda3

Simeng Jing, Qijun Zhao, Guoqing Zhao

Flight Science and Technology, School of Engineering, University of Liverpool, Liverpool, UK.

Japan Aerospace Exploration Agency


1Ryoyu Systems Co., Ltd.; Tokyo University of Agriculture and Technology2Japan Aerospace Exploration Agency3Tokyo University of Agriculture and Technology

Nanjing University Of Aeronautics And Astronautics



Rotorcraft Design 3 Advanced Concepts 2 Unmanned Systems 3 Aerodynamics 4 Aerodynamics 5

11:30

Development of Surrogate-based Design Framework for Composite Rotor Blade

Deep Vision Based Photogrammetry System for Rotor Blade Motion and Deflection Measurements

Assessment Of Fault Tolerant Estimation For Light Utility Helicopter Dynamics

Main Rotor – Tail Rotor Interactional Noise

Aerodynamic design optimization of helicopter rotor airfoil

Dawoon Lee1, Jaesung Bae2, Sungnam Jung2, Kwanjung Yee1

Giray Yillikci1, Yavuz Güleç2, Oğuz Şahin2, Muhammed Emre Bilen2

Özlem Dökme1, Chingiz Hajiyev2

Mehmet Melih Atalay1, Murat Şenipek1, Arda Yücekayalı1, Yusuf Özyörük2

Onur Okumuş, Alper Ezertaş

1Department of Mechanical & Aerospace Engineering, Seoul National University, Seoul, Republic of Korea2Department of Aerospace Information Engineering, Konkuk University, Seoul, Republic of Korea

1Siemens AŞ, Istanbul, TURKEY2Turkish Aerospace Industries Inc.

1 Turkish Aerospace Industries Inc.2Faculty of Aeronautics and Astronautics, Istanbul Technical University, İstanbul, TURKEY

1Turkish Aerospace Industries Inc.2Middle East Technical University,Ankara,Turkey


12:00

Student Competition Team Presentation: Caladrius, VFS Student Competition 2019 winner

Evaluation of Surrogate-Based Modeling Methods for the Optimization of Helicopter Rotor Structures for Minimum Vibration

Preliminary Design of a Set of Airfoils Applied to Coaxial Rotors

Tip vortex structure research for the isolated helicopter`s main rotor model

Seyhan Gül (Team Captain) M. Emre Bilen1, Ender Cigeroglu2, H. Nevzat Özgüven2

Xin Yuan, Qi Jun Zhao, Si Meng Jing

Liia Makarova1, Vladimir Pakhov2, Robert Stepanov2

Maryland University 1 Turkish Aerospace Industries Inc.2Middle East Technical University

College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics

1Nanjing University of Aeronautics and Astronautics, Nanjing, China2Kazan National Research Technical University named after A.N.Tupolev - KAI, Kazan, Russia

12:30 Lunch

13:30 Invited Speaker - Dr. Elif Ahci (Airbus Helicopters Inc, Head of Dynamic Systems Germany): Latest Rotor Developments in Helicopter Industry

14:00 Invited Speaker - Mr. Mike Hirschberg (Vertical Flight Society) : The Electric VTOL Revolution

14:30 ERF2018 Best Paper Presentation: Simulation Tools for UAV/OPV Autorotation Performance Metrics Evaluation Laurent Binet (ONERA), Christian Brackbill, David Quinn (AMRDEC)

15:00 Coffee Break




Rotorcraft Design 4 Aerodynamics 6 Rotorcraft Design 5 Aerodynamics 7 Propulsion and Drive 2

15:30

TOROS Model Linearization by Subspace Identification

Comparison between a tractor type-propeller and a pusher-type propeller for Mars airplane

Mission-based Optimal Morphing Parameters for Rotors with Combined Chord and Twist Morphing

Airwake Investigations on SFS2 with a Hovering Helicopter Rotor by Computational Fluid Dynamics Simulations

Design of an Experimental Setup for Periodic Forced Response Analysis of Shrouded Blades with Frictional Contacts

Sevil Avcioglu, Yusuf Onur Arslan

Koichi Yonezawa1, Tomonori Kagayama2, Shigeru Sunada3, Kazuyasu Sugiyama2

Rohin Kumar Majeti1, Stephan Benz2

Ezgi Orbay, Nilay Sezer Uzol Eren Öney, Ender Cigeroglu


1Central Research Institute of Electric Power Industry, Abiko, Japan2Osaka University, Toyonaka, Japan3Nagoya University, Nagoya, Japan

1Rotorcraft, Institute of Flight Systems, German Aerospace Center (DLR), Braunschweig, Germany2Department of Mechanical and Aerospace Engineering, Technical University, Braunschweig, Germany

Dept. of Aerospace Engineering, METU, Ankara, Turkey

Middle East Technical University

16:00

Analysis on radar scattering characteristics of helicopter based on finite-volume time-domain method

A Numerical Study on Aerodynamic Interference from Different Configurations of Helicopter Emergency Float

A summary of rotary-wing SIL activities: Flight Mechanics & Control Perspective

Influence of Rotor Blade Twist on the Ducted Rotor Performance

Surrogate Model Based Concept Exploration with Small Helicopter Case Study

Yongmeng Jiang, Bo Wang, Qijun Zhao, Xiangwen Jiang

Zhi Sun1, Jianhong Sun1, Qijun Zhao2, Mingqi Li3, Xing Guo1

Umut Türe, Ilgaz Doğa Okcu Yasutada Tanabe1, Hideaki Sugawara2, Koichi Yonezawa3, Shigeru Sunada4, Hiroshi Tokutake5

Alperen Yillikci1, Mustafa Emre Gündüz2, Hasan İbaçoğlu2

National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics,Nanjing, Jiangsu, China

1Key Laboratory of Aircraft environment control and life support MIIT, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China2National Key Laboratory of Rotorcraft Aerodynamics, Nanjing University of Aeronautics & Astronautics, Nanjing 210016,China3Aviation Key Laboratory of Science and Technology on Life-support Technology, Xiangyang, 441003, China


1Japan Aerospace Exploration Agency (JAXA)2Ryoyu Systems Co. Ltd.3Central Research Institute of Electrical Power Industry4Nagoya University5Kanazawa University

1 TAI GmbH, Hamburg, Germany 2 Turkish Aerospace Industries Inc.



Rotorcraft Design 4 Aerodynamics 6 Rotorcraft Design 5 Aerodynamics 7 Propulsion and Drive 2

16:30

Automatic Interface Testing By Using Ballard Copilot

Numerical and Experimental Investigation of Rotor Aerodynamics In Ground Effect with Inclined Planes

Design of the Maryland Tiltrotor Rig Hingeless Hub

Computational Analysis of Advanced Geometry Rotor Blades

Experimental Verification Of İmprovements İn Static And Fatigue Bending Capacity Of Spur Gear Tooth Via Tooth Root Design Optimization

Ismail Şimşekoğlu, Abdullah Vural

Mehmet Şahbaz, Nilay Sezer Uzol, Dilek Funda Kurtuluş

Seyhan Gul, Anubhav Datta Yunus Emre Serttaş1, Mehmet Özgünoğlu2, Özge Özdemir1

Nihat Yıldırım1, Fatih Erdoğan2, Mert Vardar2


Department of Aerospace Engineering /METU/Ankara/Turkey

University of Maryland, College Park, Maryland, 20742, U.S.A.

1Istanbul Technical University2Gumush Aerospace and Defence

1Gaziantep University, Gaziantep/TURKEY 2AeroGDT Inc., Ankara/TURKEY

17:00

Agility Assessment of Utility & Attack Configurations

Rotor Aerodynamics and Performance Enhancement via Active Trailing Edge Flaps

Multibody Simulation of Helicopter Rotor with Flexible Blade and Hub

Design of A Hover Test Stand and Performance Enhancement of Actively Controlled Blades

Murat Şenipek, Arda Yücekayalı, Yüksel Ortakaya

Hüseyin Ural, Özge Özdemir Ihsan Bali Ozturan1, Altan Kayran2

Yunus Emre Serttaş, Onur Taştan, Hüseyin Ural, Merve Şahin, Özge Özdemir, Okşan Nuriye Leman Çetiner Yıldırım, Metin Orhan Kaya


Istanbul Technical University, Faculty of Aeronautics and Astronautics

1 Turkish Aerospace Industries Inc.2Professor in Aerospace Engineering, Middle East Technical University, Ankara, Turkey

Istanbul Technical University, Faculty of Aeronautics and Astronautics

17:30 Best Paper Award and Closing Ceremony

18:30 End of Forum

final program - arf 2019final program 8th asian/australian rotorcraft forum october 30 - november 2...

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