| Tuesday, 05. September 2023 | |||||
| City Hall | Großer Rathaussaal | City Hall | Le-Theule-Saal | City Hall | Neuer Ratssaal | Helicopter Museum | Eventraum | Helicopter Museum | Archivraum | |
| 08:00 - 09:00 | Registration open |
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| 09:00 - 10:30 | Opening Ceremony N.N., Confernce opening with Welcome Adresses |
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| 10:30 - 11:00 | Networking and Refreshmentbreak |
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| 11:00 - 11:30 | Plenary Lecture 1 - Chair: K. Pahlke, DLR Stefan Levedag, Director of the Institute of Flight Systems Technology at German Aerospace Center (DLR), Rotorcraft Research at German Aerospace Center (DLR) – Science and Application |
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| 11:30 - 12:00 | Plenary Lecture 2 - Chair: K. Pahlke, DLR Rainer Heeger, Research Program Manager at Airbus Helicopters , Airbus vision for the future of vertical flight |
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| 12:00 - 12:30 | Plenary Lecture 3 - Chair: K. Pahlke, DLR Philippe Petit, Research Engineer at Institute of Flight Systems at German Aerospace Center (DLR) | VFS Best paper Award Winner 2023, Validation of a Motion Sickness Prediction Model via Flight Tests on DLR's Bo-105 Helicopter |
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| 12:30 - 13:30 | Networking Lunch |
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| 13:30 - 15:30 | 1.1 Aerodynamics 1: Airfoil Characteristics | 2.1 Acoustics 1: Propeller | 3.1 Dynamics 1: Methods | 4.1 Flight Mechanics 1: flow modelling | 5.1 Crew Station 1 |
| 15:30 - 16:00 | Networking and Refreshmentbreak |
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| 16:00 - 17:30 | 1.2 Aerodynamics 2: Multirotors | 2.2 Aircraft Design 1 | 3.2 Dynamics 2: Whirlflutter | 5.2 Engine & Propulsion | |
| 18:00 - 21:00 | Welcome Reception @ Helicopter Museum Bückeburg |
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| Wednesday, 06. September 2023 | |||||
| City Hall | Großer Rathaussaal | City Hall | Le-Theule-Saal | City Hall | Neuer Ratssaal | Helicopter Museum | Eventraum | Helicopter Museum | Archivraum | |
| 08:30 - 09:00 | Registration open |
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| 09:00 - 10:30 | 1.3 Aerodynamics 3: Methods | 2.3 Acoustics 2: Rotor | 3.3 Dynamics 3: Loads | 4.3 Flight Mechanics 2: Fl. Dyn. Modelling | 5.3 UAM 1 |
| 10:30 - 11:00 | Networking and Refreshmentbreak |
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| 11:00 - 11:45 | Plenary Lecture 4 - Chair: K. Pahlke, DLR Luca Medici, Head of Aircraft System Integration at Leonardo Helicopter Division, Advancing Air Mobility – New Paradigms and Lessons Learned |
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| 11:45 - 12:30 | Conference Foto , Meeting of the participants of the ERF for a group photo at the Helicopter Museum |
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| 12:30 - 13:30 | Networking Lunch |
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| 13:30 - 15:30 | 1.4 Aerodynamics 4: Active Rotors | 2.4 Aircraft Design 2: Concept Design | 3.4 Test & Evaluation 1 | 4.4 Flight Mechanics 3 | 5.4 Crew Station 2 |
| 15:30 - 16:00 | Networking and Refreshmentbreak |
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| 16:00 - 17:30 | 1.5 Aerodynamics 5: Windtunnel Test | 2.5 Aircraft Design 3: Config. | 3.5 Dynamics 4: Vibration Reduct. | 4.5 Unmanned Rotorcraft 1 | 5.5 Certification by Simulation 1 |
| 19:00 - 23:00 | Conference Dinner @ Schloss Bückeburg (Registration required!) |
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| Thursday, 07. September 2023 | |||||
| City Hall | Großer Rathaussaal | City Hall | Le-Theule-Saal | City Hall | Neuer Ratssaal | Helicopter Museum | Eventraum | Helicopter Museum | Archivraum | |
| 09:00 - 10:30 | 1.6 Aerodynamics 6: Coaxial Rotors | 2.6 Acoustics 3: Toolchains | 3.6 Dynamics 5 | 4.6 Flight Mechanics 4 | 5.6 Certification by Simulation 2 |
| 10:30 - 11:00 | Networking and Refreshmentbreak |
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| 11:00 - 11:45 | Plenary Lecture 6 - Chair: K. Pahlke, DLR David Solar, European Union Aviation Safety Agency, Certification of eVTOL – Status and outlook |
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| 11:45 - 12:30 | Plenary Lecture 7 - Chair: K. Pahlke, DLR Torsten Kasper, Army Concepts and Capability Development Center , Future platforms and operations – a view on german army aviation |
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| 12:30 - 13:30 | Networking Lunch |
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| 13:30 - 15:30 | 1.7 Aerodynamics 7: Appl./Eval. | 2.7 UAM 2 | 3.7 Test & Evaluation 2 | 4.7 Unmanned Rotorcraft 2 | 5.7 Structures and HUMS 1 |
| 15:30 - 16:00 | Networking and Refreshmentbreak |
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| 16:00 - 17:30 | 1.8 Aerodynamics 8: Performance | 2.8 Aircraft Design 4: Components | 3.8 Dynamics 6 | 4.8 Unmanned Rotorcraft 3 | 5.8 Structures and HUMS 2 |
| 17:30 - 17:31 | End of ERF2023 |
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| 13:30 | 14:00 | 0001 |
Factors affecting Rotor Stall Computation by Comprehensive Rotor Codes B.G. van der Wall, German Aerospace Center (DLR), Germany | ||||
| 14:00 | 14:30 | 0099 |
An Innovative CFD Methodology for Evaluation of Airfoils Aerodynamic Characteristics F. Manara, G. Frassoldati, Leonardo Helicopters Division, Università degli Studi Roma Tre, Italy; D. Malacrida, Leonardo Labs, Italy; S. Platzer; Leonardo Helicopters Division, Italy | ||||
| 14:30 | 15:00 | 0109 |
Aerodynamic Analysis of Rotor Airfoils with Camber Morphing Mechanism versus Plain Flaps A. Abdelmoula, F. Grimm, I. Yavrucuk, J. Rauleder, Georgia Institute of Technology, United States; Technical University of Munich, Germany | ||||
| 15:00 | 15:30 | 0117 |
Drone Rotor Performance under Icing Conditions A. Gupta, Linde Inc., United States; A. Gahlot, L.N. Sankar; Georgia Institute of Technology, United States | ||||
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| 13:30 | 14:00 | 0020 |
CFD Validation for eVTOL Propeller Performance and Acoustics G. Qiao, G.N. Barakos; University of Glasgow, United Kingdom | ||||
| 14:00 | 14:30 | 0024 |
Investigation of the Ducted-Propeller Effects on Aeroacoustic Performance using Phase-Locked PIV J. Sun, K. Yonezawa, Central Research Institute of Electric Power Industry, Japan; H. Liu; Chiba University, Japan | ||||
| 14:30 | 15:00 | 0057 |
Assessment of Aeroacoustic Optimisation Schemes for a Tilt-Propeller Application in Hover and Cruise O. Bergmann, F. Möhren, D. Frey, F. Janser, C. Braun; FH Aachen University of Applied Sciences, Germany | ||||
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| 13:30 | 14:00 | 0132 |
Rotor Loads Prediction via Virtual Sensors - Blending Physics and AI F. Midei, A.A. Trezzini, M. Zilletti, C. Sbarufatti; Politecnico di Milano, Italy ;Leonardo, Italy | ||||
| 14:00 | 14:30 | 0135 |
Machine Learning Based Approaches for Estimating Rotor Airloads in Hover H. Lee, P. Mortimer, P. Seshadri, J. Sirohi, J. Rauleder; Georgia Institute of Technology, United States ;The University of Texas at Austin, United States | ||||
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| 13:30 | 14:00 | 0004 |
Comparison of different Inflow Models for Intermeshing Rotors T. Ehlert, F. Guner, A.E. Voigt; DLR Institute of Flight Systems, Germany | ||||
| 14:00 | 14:30 | 0163 |
System Identification of E-VTOL Rotor in Vortex Ring State by Viscous Vortex Particle Method M. Senipek, I.D. Okcu, O. Tekinalp, K. Leblebicioglu; Turkish Aerospacec, Turkey ;Middle East Technical University, Turkey | ||||
| 14:30 | 15:00 | 0005 |
An Efficient Helicopter Main Rotor Trim Method based on Computational Fluid Dynamics J. Fu, L. Vigevano; Politecnico di Milano, Italy Presenter: Luigi Vigevano, Politecnico di Milano | ||||
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| 13:30 | 14:00 | 0076 |
Effect of a Haptic Torque Protection with an Active Sidestick on Pilot\'s Eyes-Out Capability during a Helicopter Takeoff M. Müllhäuser, DLR, Institut für Flugsystemtechnik, Germany | ||||
| 14:00 | 14:30 | 0101 |
Usability Analysis and UX Design Recommendations for an Enhanced User Experience of O.R.I.O.N, , the Technical Documentation Digital Viewing Platform M. Faye, N. Jahchan; Airbus Helicopters, France | ||||
| 14:30 | 15:00 | 0120 |
Analysis of Multimodal Signal in Rotorcraft Cockpit D. Marchesoli, M.S. Lukasiewicz, C. Talamo, A. Zanoni, P. Masarati; Politecnico di Milano, Italy | ||||
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| 16:00 | 16:30 | 0006 |
High-fidelity Aerodynamic and Acoustic Evaluations of a Heavy-lift eVTOL in Hover T. Zhang, University of Leicester, United Kingdom; G.N. Barakos, University of Glasgow, United Kingdom | ||||
| 16:30 | 17:00 | 0081 |
Variable Rotor Speed Trim and Interactional Aerodynamics for Quadcopter UAS J.W. Lim, US Army, United States; A.D. Thai, Joby Aviation, United States | ||||
| 17:00 | 17:30 | 0105 |
Multi-Rotor Wake Interaction Characterization F. De Gregorio, K.-S. Rossignol, G. Ceglia, J. Yin; CIRA, Italy ;DLR, Germany | ||||
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| 16:00 | 16:30 | 0046 |
Automated Calculation of the Internal Structure and the Natural Frequencies of Helicopter Rotor Blades with Regard to Automated Rotor Blade Optimization F. Becker, S. Kalow, R. Bartels; German Aerospace Center (DLR), Germany | ||||
| 16:30 | 17:00 | 0052 |
Development and Application of Improved Tandem Neural Networks for Inverse Design of Rotorcraft Airfoil A. Anand, K. Marepally, B. Lee, J.D. Baeder; University of Maryland, United States | ||||
| 17:00 | 17:30 | 0175 |
Trajectory Modelling of Transition Regime Using Blade Element Method for Different eVTOL Aircraft Configurations S.K.Y. Lim, Z.Y. Boon, J. Wang; Nanyang Technological University Singapore, Singapore Presenter: Shawn Lim Kin Yip, Nanyang Technological University | ||||
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| 16:00 | 16:30 | 0072 |
Whirl Flutter Predictions for Distributed Tiltrotor Configurations S. Gul, Science and Technology Corporation, United States; H. Yeo, U.S. Army, United States | ||||
| 16:30 | 17:00 | 0102 |
Whirl Flutter Analysis of a Tiltrotor Semi-Span Wind Tunnel Model for Test Results Correlation J. Montaño-Oliveros, F. Fonte, S. van't Hoff, B. Timmerman; Leonardo Helicopters, Italy ;Royal Netherlands Aerospace Centre, Netherlands | ||||
| 17:00 | 17:30 | 0162 |
A Minimum Complexity Model for the Aeroelastic Analysis of Distributed Propulsion Aircraft A. Tamer, University of Bath, United Kingdom; A. Tatar, Leonardo Helicopters, United Kingdom Presenter: Ali Tatar, Leonardo Helicopters | ||||
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| 16:00 | 16:30 | 0065 |
Engine Air Intake Design and Evaluation - Examples from the Bluecopter™ Demonstrator. A. Garavello, T. Kneisch, M. Müller, A. D'Alascio; Airbus Helicopters Deutschland GmbH, Germany | ||||
| 16:30 | 17:00 | 0148 |
Effects of Aero-Propulsive Coupling on High Solidity Electric Ducted Fan Performance for Various Wing Integrations D.A. Safieh, J. Rauleder; Georgia Institute of Technology, United States | ||||
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| 09:00 | 09:30 | 0031 |
Validation of a New Solver based on the Vortex Particle Method for Wings, Propellers and Rotors J. Valentin, L. Bernardos; ONERA, France | ||||
| 09:30 | 10:00 | 0113 |
Detached-Eddy Simulation of UH-60A Airloads using an Immersed Boundary Method J.H. Park, D. Linton, B. Thornber; The University of Sydney, Australia | ||||
| 10:00 | 10:30 | 0152 |
Validation of a Mid-Fidelity CFD/CSD Coupling using the Lattice-Boltzmann Method B. Horvat, I. Yavrucuk; Institute. f. Helicopter Technology, Technical University Munich, Germany | ||||
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| 09:00 | 09:30 | 0085 |
Validation of a Surrogate-Based Methodology for Low-Noise UAV/UAM Rotor Design A. Sieradzki, P. Kekus, W. Klimczyk; Lukasiewicz Research Network, Institute of Aviation, Poland | ||||
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| 09:00 | 09:30 | 0063 |
Rapid Dynamic Load Estimation Procedure for Lifting Propellers in Forward Flight F. Möhren, O. Bergmann, F. Janser, C. Braun, K.-U. Schröder, RWTH Aachen University, Germany; FH Aachen, Germany | ||||
| 09:30 | 10:00 | 0142 |
An Exploration of Rotor System Component Loads of the NRC Bell412 Advanced Systems Research Aircraft due to Variations in Flight Control Augmentation M. Alexander, National Research Council Canada / Flight Research Laboratory, Canada | ||||
| 10:00 | 10:30 | 0112 |
Direct Load Recognition to Estimate the Damper Load on the H175 Fleet C. Del cistia Gallimard, Airbus Helicopters / Sorbonne Université, France; K. Nikolajevic, F. Beroul, J. Denoulet, B. Granado, C. Marsala; Airbus Helicopters, France ;Sorbonne Université, France | ||||
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| 09:00 | 09:30 | 0044 |
Flight Dynamic Modeling and Stability of a Small-Scale Side-By-Side Helicopter for Urban Air Mobility F. Mazzeo, D. Fattizzo, G. Bertolani, E.L. de Angelis, F. Giulietti, F. Leali, M.D. Pavel, Delft Technical University, Netherlands; University of Modena and Reggio Emilia, Italy ;University of Bologna, Italy | ||||
| 09:30 | 10:00 | 0078 |
Metrics and Guidelines for Rotorcraft Modeling Accuracy and their Relation to Model Uncertainty: A State-of-the Practice Survey M.D. Pavel, A. Aba, P. Capone, ZURICH University of Applied Sciences, Switzerland; Delft University of Technology, Netherlands | ||||
| 10:00 | 10:30 | 0093 |
Vibrational Stability Effects in Rotorcraft Flight Dynamics U. Saetti, University of Maryland, United States; Z. Chen, J.F. Horn, T. Berger, U. S. Army , United States; Penn State , United States | ||||
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| 09:00 | 09:30 | 0061 |
Technology Requirements for the Development of Aircraft for Urban Air Mobility - Status Quo B. Lukic, U. Durak; German Aerospace Center (DLR), Germany | ||||
| 09:30 | 10:00 | 0103 |
Do VTOL Aircraft create an inherently more Problematic Downwash than Conventional Helicopters? R.E. Brown, Sophrodyne Aerospace, United Kingdom | ||||
| 10:00 | 10:30 | 0115 |
Stochastic Aeroelastic Analysis of eVTOL Aircraft S. Murugan, IIT Madras, India | ||||
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| 13:30 | 14:00 | 0017 |
Simulation of Active Twist Rotor Blades using a Thermal Analogy Method in HMB3 R. Steininger, G.N. Barakos, M.A. Woodgate; University of Glasgow, United Kingdom | ||||
| 14:00 | 14:30 | 0075 |
Investigations of a Boxed Rotor: The STAR II Rotor in DLR’s Test Hall. G. Wilke, DLR AS-HEL, Germany; H. Sugawara, T. Yasutada, O. Schneider, B.G. van der Wall; JAXA, Japan ;DLR FT-HUB, Germany | ||||
| 14:30 | 15:00 | 0121 |
Fluid Structure Interaction Investigation of the Aerodynamic Characteristics of a Dynamic Camber Morphing and Pitching Rotor Airfoil M.-K. Yurt, A. Abdelmoula, J. John, I. Yavrucuk; Technical University of Munich, Germany | ||||
| 15:00 | 15:30 | 0150 |
Towards Active Rotor Analysis using Viscous Vortex Particle Method S. Kumar, J. Rauleder, Georgia Tech, United States; I. Yavrucuk; TU Munich, Germany | ||||
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| 13:30 | 14:00 | 0016 |
Concept Study of a Fast VTOL-UAV Technology-Demonstrator for MUM-T A. Štrbac, A.E. Voigt, D.H. Greiwe, P. Weiand, R. Bartels, M. Müller, J. Schmiedel, M. Meunier, U.T.P. Arnold, J. Litzba; German Aerospace Center (DLR), Germany ;Airbus Helicopters Technik GmbH (AHTech), Germany | ||||
| 14:00 | 14:30 | 0032 |
A Comparison of three Conceptual Design Approaches applied to an Electric Distributed Lift Aircraft J.M. Vegh, R. Scott, P.-M. Basset, R. Perret, N. Beals, R. Singh; U.S. Army DEVCOM Aviation and Missile Center, United States ;ONERA – The French Aerospace Lab, France ;U.S. Army DEVCOM Army Research Lab, United States | ||||
| 14:30 | 15:00 | 0040 |
Rotorcraft Fuselage Drag Estimation Method for Conceptual Design Phase F. Yilmaz, A.E. Coskun, H. Ibacoglu, M. Kilcik, T. Kayabasi; Turkish Aerospace Industries, Turkey | ||||
| 15:00 | 15:30 | 0064 |
Rotor Aeroelastic Stability Assessment in the New Coral Framework C. Pasquali, N. Spyropoulos, R. Leibbrandt, M. Gennaretti, V.A. Riziotis, S. Radler, G. Bernardini, G. Papadakis; Universita degli studi di Roma Tre, Italy ;National Technical University of Athens, Greece ;Kopter Germany GmbH, Germany | ||||
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| 13:30 | 14:00 | 0002 |
Engine Back-up System in Flight Test Campaigns: a new Approach to the Height-Velocity Diagram Demonstration S. Taheri, A. Delavet; Airbus Helicopters, France | ||||
| 14:00 | 14:30 | 0013 |
Development of the UK National Rotor Rig for Aeroelastic Testing of Rotary Wings D. Zagaglia, A.D. Croke, R.B. Green, G.N. Barakos; University of Glasgow, United Kingdom | ||||
| 14:30 | 15:00 | 0029 |
Icing and De-icing under Centrifugal Load in DLR’s Whirl Tower Facility S. Kalow, R. Bartels, O. Schneider, D. Sahyoun, R. Keimer; German Areospace Center (DLR), Germany | ||||
| 15:00 | 15:30 | 0030 |
Holographic Visual Cues for Mission Task Elements T. Jusko, C. Walko, L. Kante, TU Dresden, Germany; German Aerospace Center (DLR), Germany Presenter: Tim Jusko, DLR | ||||
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| 13:30 | 14:00 | 0077 |
Rotor Control Equivalent Turbulence Input (RCETI) Models for Multi-Rotor Vehicles M.A. Hayajnh, Georgia Institute of Technology, United States; J.V.R. Prasad, Georgia Institute of Technology , United States | ||||
| 14:00 | 14:30 | 0100 |
Retracting Blade Stall Phenomenon - Review of Investigations Performed during the PZL W-3A Serial and New Blade Projects J. Malecki, M. Pokwapisz; “PZL-Swidnik” S.A. Leonardo Helicopters Company, Poland | ||||
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| 13:30 | 14:00 | 0147 |
Convertiplane Control during Transition: the Collective and Throttle Lever (CATL) A. Abà, A. Pedrioli, R. Monstein, M. Hitz, G. Schneider, P. Capone; ZHAW, Switzerland | ||||
| 14:00 | 14:30 | 0137 |
Spatial Audio Cueing Algorithms for Augmented Pilot Perception in Degraded/Denied Visual Environments M.T. Morcos, S.M. Fishman, U. Saetti, T. Berger, U.S. Army Combat capabilities DEVCOM, United States; M. Godfroy-Cooper, E.N. Bachelder; University of Maryland, United States ;San Jose State University, United States | ||||
| 14:30 | 15:00 | 0090 |
The Impact of the Installation of Digital Avionics Equipment on the Power Consumption of the Helicopter P. Stronikowski, PZL-Swidnik S.A., Poland | ||||
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| 16:00 | 16:30 | 0014 |
Experimental Investigation into the Onset of Stall Flutter on Tiltrotor Blades A.D. Croke, D. Zagaglia , M.A. Woodgate, R.B. Green, G.N. Barakos; University of Glasgow, United Kingdom | ||||
| 16:30 | 17:00 | 0173 |
Experimental Study on Aerodynamic Drag of Booms and Boom Mounted Stationary Rotors on eVTOL Aircraft P.J.K. Koh, S.K.Y. Lim, J. Wang; Nanyang Technological University Singapore, Singapore Presenter: James Wang, eVTOL Research and Innovation Centre | ||||
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| 16:00 | 16:30 | 0054 |
Modelling and Simulation of a Novel Bioinspired Flapping-Wing Rotary MAV X. Huang, L. Lu, J. Whidborne, S. Guo; Cranfield University, China | ||||
| 16:30 | 17:00 | 0098 |
A Weight Prediction Model for Electric Propulsion System applied on Light Helicopters (CS.27) F.L.C. Mauri, F. Merlo, G. Tramontana; Leonardo S.p.A., Italy | ||||
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| 16:00 | 16:30 | 0066 |
Optimal Deployment Schedule for Vibration Reduction of Lift-Offset Coaxial Rotorcraft using Individual Blade Control S.H. Hong, D.K. Kim, S.N. Jung; Konkuk University, South Korea | ||||
| 16:30 | 17:00 | 0082 |
An Integrated Three-Dimensional Aeromechanical Analysis for the Prediction of Stresses on Lift Offset Coaxial Rotors M. Patil, R. Lumba, B. Jayaraman, A. Datta; UNIVERSITY OF MARYLAND, United States ;U.S. Army, United States | ||||
| 17:00 | 17:30 | 0095 |
Feasibility and Effectiveness of a Higher Harmonic Control System for a Medium Utility Helicopter D.-H. Kim, Korea Aerospace Research Institute, South Korea; J.-S. Park, S.-W. Bang; Chungnam National University, South Korea | ||||
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| 16:00 | 16:30 | 0012 |
Using Time-to-contact as a Flight Control Parameter to Improve Rotary-Wing UAS Ship Deck Landings C. Dadswell, M. Jump; University of Liverpool, United Kingdom | ||||
| 16:30 | 17:00 | 0018 |
An Improved Method for Swing State Estimation in Rotorcraft Slung-Load Applications E.L. de Angelis, F. Giulietti; University of Bologna, Italy | ||||
| 17:00 | 17:30 | 0019 |
Cooperative Transportation of a Cable-Suspended Load using Rotorcraft: A Minimal Swing Approach E. Costantini, E.L. de Angelis, F. Giulietti; University of Bologna, Dept. of Industrial Engineering (DIN), Italy | ||||
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| 16:00 | 16:30 | 0127 |
Rotorcraft Flight Simulation to support Aircraft Certification: A Review of the State of the Art with an Eye to Future Applications A. Rylko, S. van't Hoff, NLR, Netherlands; L. Lu, Cranfield University, United Kingdom; G. Padfield, P. Podzus, DLR, Germany; M. White, G. Quaranta; Politecnico di Milano, Italy ;University of Liverpool, United Kingdom Presenter: Giuseppe Quaranta, Politecnico di Milano | ||||
| 16:30 | 17:00 | 0087 |
Case Studies to illustrate the Rotorcraft Certification by Simulation Process; CS 29/27 Low-Speed Controllability S. van 't Hoff, Royal Netherlands Aerospace Centre, Netherlands; M. White, C. Dadswell, L. Lu, Cranfield University, United Kingdom; G. Padfield, G. Quaranta, Politecnico di Milano, Italy; P. Podzus, German Aerospace Centre, Germany; University of Liverpool, United Kingdom | ||||
| 17:00 | 17:30 | 0124 |
Case Studies to Illustrate the Rotorcraft Certification by Simulation Process; CS 29/27 Category A Rejected Take-Off, Confined Area M. White, C. Dadswell, G. Padfield, S. Van't Hoff, R. Bakker, L. Lu, Cranfield University, United Kingdom; G. Quaranta, Politechnico di Milano, Italy; P. Podzus, DLR, Germany; The University of Liverpool, United Kingdom ;Royal Netherlands Aerospace Centre, NLR, Netherlands Presenter: Mark White, The University of Liverpool | ||||
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| 09:00 | 09:30 | 0034 |
Comparing 3D and 2D CFD for Mars Helicopter Ingenuity Rotor Performance Prediction W.J.F. Koning, B.G. Allan, NASA Langley Research Center, United States; E.A. Romander, W. Johnson; NASA Ames Research Center, United States | ||||
| 09:30 | 10:00 | 0141 |
Vibration Reduction of Coaxial Rotor by Blade Installation Phase Angle T. Yumino, H. Sugawara, Y. Tanabe, M. Kameda; Tokyo University of Agriculture and Technology, Japan ;Japan Aerospace Exploration Agency, Japan | ||||
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| 09:00 | 09:30 | 0026 |
A Comprehensive Helicopter Acoustic Modeling Tool based on Simulation and Experiment F. Guntzer, J. Caillet, C. Cariou, J.-P. Pinacho, P. Dieumegard, E. Roca León; Airbus Helicopters, France | ||||
| 09:30 | 10:00 | 0080 |
Acoustic and Aerodynamic Evaluation of DLR Small-Scale Rotor Configurations within GARTEUR AG26 J. Yin, F. De Gregorio, K.-S. Rossignol, L. Rottmann, G. Ceglia, G. Reboul, French Aerospace Center - ONERA, France; G. Barakos, G. Qiao, M. Muth*, M. Kessler*, A. Visingardi, M. Barbarino, F. Petrosino, A. Zanotti, N. Oberti, L. Galimberti, G. Bernardini, C. Poggi, L. Abergo, F. Caccia; German Aerospace Center - DLR, Germany ;Italian Aerospace Research Center - CIRA, Italy ;University of Glasgow, United Kingdom ;*University of Stuttgart, Germany ;Politecnico di Milano, Italy ;Roma Tre University, Saudi Arabia ;King Abdullah University of Science and Technology - KAUST, Saudi Arabia | ||||
| 10:00 | 10:30 | 0126 |
Deep Learning Surrogate Model for Rotorcraft Aeroacoustic Simulations using a Geodesic Convolutional Network B. Erwee, A. Scandroglio, N. Sanguini, T. Benacchio, F. Di Cintio; Leonardo Helicopters, United Kingdom | ||||
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| 09:00 | 09:30 | 0009 |
Possibilistic Uncertainty Quantification for Parametrically Reduced Models of Dynamic Systems with Many Inputs L. Frie, T. Könecke, M. Hanss, P. Eberhard; ITM University of Stuttgart, Germany | ||||
| 09:30 | 10:00 | 0131 |
Wind Tunnel Test of a Single Electrical Lift Thrust Unit to assess Static and Dynamic Loads M. Zilletti, D. Prederi, R. Costantini, M. Zaccara, M. Ricciardi, G. Morelli, Politecnico di Miano, Italy; P. Masarati, Politecnico di Milano, Italy; Leonardo, Italy | ||||
| 10:00 | 10:30 | 0157 |
Comfort Assessment in Urban Air Mobility Vehicles A. Tamer, University of Bath, United Kingdom; A. Zanoni, P. Masarati; Politecnico Di Milano, Italy | ||||
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| 09:00 | 09:30 | 0149 |
Effect of Torsional Flexibility on an Unmanned Helicopter Performance Including Compressibility Effect A.F. Uzunkaya, ASELSAN, Middle East Technical University, Turkey; Y. Yaman, Middle East Technical University, Turkey | ||||
| 09:30 | 10:00 | 0166 |
AW09 Tail Rotor System Control Authority Assessment S. Bölk, A. Masi, F. Scorcelletti; Kopter Group AG, Switzerland Presenter: Sören Bölk, Kopter Group AG | ||||
| 10:00 | 10:30 | 0167 |
Flight Trajectory Tracking for a Helicopter in Tail Rotor Failure Y.O. Arslan, I.D. Okcu; Turkish Aerospace, Turkey | ||||
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| 09:00 | 09:30 | 0033 |
Case Studies to illustrate the Rotorcraft Certification by Simulation Process; CS 27/29 Dynamic Stability Requirements L. Lu, Cranfield University, United Kingdom; G. Padfield, M. White, C. Dadswell, G. Quaranta, Politecnico di Milano, Italy; S. van’t Hoff, Royal Netherlands Aerospace Centre, Netherlands; P. Podzus, German Aerospace Center, Germany; University of Liverpool, United Kingdom | ||||
| 09:30 | 10:00 | 0128 |
Rotorcraft Flight Simulation so support Aircraft Certification: Methodologies to Evaluate the Uncertainties on a Tiltrotor Model M. Daniele, M. Mamino, G. Quaranta; Politecnico di Milano, Italy Presenter: Matteo Daniele, Politecnico di Milano | ||||
| 10:00 | 10:30 | 0145 |
Virtual-Pilot-in-the-Loop Simulation Model to assess Helicopter Routes Feasibility F. Roncolini, G. Quaranta; Politecnico di Milano, Italy | ||||
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| 13:30 | 14:00 | 0007 |
Coupled Ship Airwake and Rotor Airloads Simulation Methodology G. Frassoldati, Leonardo S.p.A., Università Degli Studi Roma Tre, Italy; C. Capizzi, D. Prederi, S. Melone; Leonardo S.p.A., Italy | ||||
| 14:00 | 14:30 | 0053 |
Actuator Surface Model and Blade Resolved Simulations of an Attack Reconnaissance Class Rotor in Hover and Forward Flight A. Coyle, B. Thornber; The University of Sydney, Australia | ||||
| 14:30 | 15:00 | 0092 |
Sensitivity of Rotor Aeroelastic Predictions with Two-Equation Turbulence Models A. Crawford, P. Sridhar, M.J. Smith; Georgia Institute of Technology, United States | ||||
| 15:00 | 15:30 | 0136 |
Evaluation of a Range of Modeling Approaches for UAV Unsteady Aerodynamics B. Oates, P. Su, J.T. Hrynuk, DEVCOM Army Research Laboratory, United States; M.J. Smith, J. Rauleder; Georgia Institute of Technology, United States | ||||
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| 13:30 | 14:00 | 0116 |
Performance, Environmental, and Mobility Analysis of Large Capacity Fast Rotorcraft Configurations for the European Regional Air Traffic Market L. Declerck, M. Cruellas Bordes, C.A. Saias, D. Nalianda, B.D.J. Schreiner, G.A. Misté, A. Dal Monte, E. Benini, A. Junior, German Aerospace Centre, Germany; Royal Netherlands Aerospace Centre, Netherlands ;Cranfield University, United Kingdom ;University of Padova, Italy Presenter: Deneys Schreiner, Cranfield University | ||||
| 14:00 | 14:30 | 0123 |
Lightning Threat on VTOLS S. Zehar, B. Tagliana, M. Meyer, P. Lalande, F. Pechereau; Airbus Helicopters, France ;ONERA, France | ||||
| 14:30 | 15:00 | 0154 |
A Nature Inspired Guidance Method for Improving Social Acceptance of Urban Air Mobility Z. Bilgin, M. Bronz, ENAC, Université de Toulouse, France; I. Yavrucuk; Technical University of Munich, Germany | ||||
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| 13:30 | 14:00 | 0036 |
Experimental and Numerical Evaluation on the Helicopter Rotor Response under the Crash Impact C. Lee, K. Kong, S.-H. Kang, M. Hwang, S. Shin; Seoul National University, South Korea | ||||
| 14:00 | 14:30 | 0074 |
Examination of Dynamic Characteristics of a CONEX Container in Dual Point Carriage from Simulation and Wind Tunnel Test Z. Chen, J.F. Horn, J. Enciu, R. Raz, A. Rosen, L. Cicolani, San Jose State Research Foundation, United States; Penn State University, United States ;Technion-Israel Institute of Technology, Israel Presenter: Joseph Horn, Penn State University | ||||
| 14:30 | 15:00 | 0091 |
RACER - Testing of Major Components M. Blacha, Airbus Helicopters, Germany; P. Burden, Hamble Aerostructures, United Kingdom | ||||
| 15:00 | 15:30 | 0143 |
Powerplant Control System Tuning Activities C. Esen, H.M. Yalcinkaya, E. Zengin, K. Sansal, A.A. Ezertas, H.E. Tarhan; Turkish Aerospace, Turkey Presenter: Can Esen, Turkish Aerospace | ||||
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| 13:30 | 14:00 | 0047 |
Comprehensive Analysis of Single and Coaxial Small UAS Propellers in Axial Forward Flight J.D. Sinsay, Science & Technology Corp., United States; L. Battey, A. Milligan; U.S. Army DEVCOM AvMC, United States | ||||
| 14:00 | 14:30 | 0069 |
Hierarchal Planning demonstrated in Autonomous Flight; Integration of the Risk-Aware Path Planner with a Sense-And-Avoid Planner on a Black Hawk Helicopter C. Goerzen, M. Takahashi, M. Whalley, G. Schulein, San Jose State University Founcation, United States; N. Mielcarek, Universities Space Research Association, United States; W. Ogden, J. Carr, C. Ott, K. Thomazios, D. Waldman; Capabilities Development, United States ;U.S. Army Combat Capabilities Development, United States | ||||
| 14:30 | 15:00 | 0071 |
Non-Linear Approach for the Unmanned, Compound Helicopter Control S. Wasniewska, S. Topczewski; WUT, Poland | ||||
| 15:00 | 15:30 | 0084 |
A Model-Based Wind Estimation Method for Unmanned Helicopter S. Nazarov, P.-O. Gutman; Technion IIT, Israel | ||||
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| 13:30 | 14:00 | 0070 |
Analytic Mixed Variational Beam Approach for Thin-Walled Composite Blades with Three-Dimensional Warpings J.S. Bae, S.N. Jung; Konkuk University, South Korea | ||||
| 14:00 | 14:30 | 0108 |
Resonance Avoidance of Variable Speed Rotors using Variable Stiffness Blades M.R. Amoozgar, V. Portapas; University of Nottingham, United Kingdom | ||||
| 14:30 | 15:00 | 0146 |
Aeroelastic Optimization of Helicopter Composite Horizontal Stabilizer Using the Superior Damping Properties of Flax Fibers J. John, L. Gaugelhofer, C. Hackner, J. Cumiskey, I. Yavrucuk; Technical University of Munich, Germany | ||||
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| 16:00 | 16:30 | 0062 |
JAXA-ONERA-DLR Cooperation: Results from Multi-Point Aerodynamic Optimization of a Rotor in Hover and Forward Flight J. Bailly, ONERA, France; G. Wilke, DLR, Germany; K. Kimura, Y. Tanabe; JAXA, Japan Presenter: Gunther Wilke, DLR | ||||
| 16:30 | 17:00 | 0104 |
Performance of Asymmetric Propellers under Varying Blade Spacing D. Usov, T. Chronis, A. Filippone; The University of Manchester, United Kingdom | ||||
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| 16:00 | 16:30 | 0050 |
Design and Manufacture of Dynamic Assemblies and Compo-Site Drive Shafts for Tiltrotor S. Barlet-Bas, F. Malburet, L. Roucoules, C. Lopez, B. Pierrel, F. Orsoni, G. Valembois, Conseil&Technique, France; NEXTEAM, France ;Arts et Métiers, France Presenter: BARLET-BAS Sébastien, NEXTEAM | ||||
| 16:30 | 17:00 | 0073 |
Mission Performance of Different Landing Gear Types in Medium Sized Twin Engine Helicopters V. Zappek, I. Yavrucuk; Institute for Helicopter Technology, Germany | ||||
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| 16:00 | 16:30 | 0160 |
Flutter Assessment of a Rotor Blade in Steady Axial Flight based on Indicial Aerodynamics J. Arnold, DLR German Aerospace Center, Germany | ||||
| 16:30 | 17:00 | 0129 |
Development of a Mid-Fidelity Aeroelastic Coupling Framework for Analyzing Rotor-Airframe Interactions M. Linder, M.K. Yurt, J. John, I. Yavrucuk; Institute for Helicopter Technology and VTOL, TU Munich, Germany | ||||
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| 16:00 | 16:30 | 0114 |
Review of Calculation Analyzes and Tests of the SW-4 SOLO Helicopter in various Configurations J. Sokarski, R. Raczynski, A. Roslowicz, W. Kanadys; „PZL-Swidnik” S.A. Leonardo Helicopters Company, Poland Presenter: Raczynski Radoslaw, „PZL-Swidnik” S.A. Leonardo Helicopters Company | ||||
| 16:30 | 17:00 | 0151 |
HIERARCHICAL DUAL LOOP ATTITUDE CONTROL FOR UNMANNED HELICOPTER G. Bertolani, A.D. Ryals, Università di Pisa, Italy; E.L. de Angelis, F. Giulietti; Università di Bologna, Italy | ||||
| 17:00 | 17:30 | 0165 |
Helicopter Control with Dynamic Inversion and Inflow Rate Estimation G. Avanzini, University of Lecce, Italy; E.L. de Angelis, D. Fattizzo, F. Giulietti; University of Bologna, Italy | ||||
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| 16:00 | 16:30 | 0156 |
Hybrid Flax Fiber-Based Helicopter Cabin Door - Static and Dynamic Testing with Digital Image Correlation L. Gaugelhofer, J. John, M. Hajek, I. Yavrucuk; Institute for Rotorcraft an Vertical Flight, TU Munich, Germany Presenter: Lukas Gaugelhofer, Institute for Rotorcraft an Vertical Flight, TU Munich | ||||
| 16:30 | 17:00 | 0079 |
Monitoring of MGB Lubrication and Cooling System based on Big Data Normality Models and Fuzzy Expert Rules A. Mechouche, M. Houles, J. Belmonte, P.-L. Maisonneuve; Airbus Helicopters, France | ||||
| 17:00 | 17:30 | 0027 |
A Time-Frequency Analysis based Filtering Policy for False Alarm Removal in Health-And-Usage Monitoring Systems J. Leoni, A. Palman, Electrical and Avionics Systems, Leonardo Helicopters Division, Italy; M. Tanelli; Politecnico di Milano, Italy | ||||