Tentative program Sunday 22 February 2015 1700 - 1930 Registration Opens – Hilton South Wharf 1800 - 1930 Congress Welcome Reception – Hilton South Wharf Monday 23 February 2015 0700-1730 Registration opens 0805-1005 Opening Plenary session, MCEC - Meeting room 212/213 1005- 1030 1030-1210 (25 min presentation inclusive of 5 minute Q&A) Congress Opening Address Congress Plenary Address Keynote Address 1 Keynote Address 2 Morning tea – Level 2 Foyer Concurrent session 1 Aerodynamics I Chair: TBA Meeting room 212 Efficient sampling strategies for the development of a flight dynamic database Michael Young Aeroelastic modelling of vertical tail buffet Oleg Levinski Optimization of a counterrotating propeller in UAV application Chao Xu Computational benchmark of commercial fluidstructure interaction software Nicholas Giannelis Structures & Materials I Chair: TBA Meeting Room 213 Design for additive manufacture: Design of computationally efficient structural micro-lattices Marten Jurg Fibre metal laminates: Linking damage modes with impact performance Adrian Orifici Computational Design of Inhibited aerospace Coatings Ivan Cole Residual stress effects in extruded wing panels on large military transport aircraft Kevin Walker Aerospace design I Chair: TBA Meeting room 216 Comparison of the size of Australian Defence Force aircrew and US Army personnel Peter Blanchonette Design of bio-inspired autonomous aircraft for bird management at sporting facilities. Brayden Muller Energy efficiency in hover: Uneven stroking versus resonance Jia Ming Kok Conceptual Design of a Mach 4 Supersonic Business Jet Cees Bil Aircraft systems (on board & offboard) I Chair: TBA Meeting room 217 Antenna system optimisation of UAS data links Samuel Dudley HUMS I Applications Chair: TBA Meeting room 218 HUMS Keynote 1 Lessons Learnt from 30 Years of RAAF F/A-18 Hornet Usage Monitoring Neil Moorhouse Theoretical Model of a Rotary Decelerator for use in Multi-rotor Aircraft Sean Morrison An Innovative Low Maintenance Data Acquisition Solution for Load Factor Capture Curtiss-Wright Design, analysis and control allocation of an over-actuated multirotor platform Robert Porter PC-9/A Edge of the Envelope Flight Testing Data Integrity Checking Procedures Trevor Mills MH-60 Droop Stop Pounding Identification Suresh Moon HUMS are NOT a Magic Bullet Graham Forsyth Tentative program 1210-1310 1310-1450 (25 min presentation) Lunch – Level 2 Foyer Concurrent session 2 Aerodynamics II Chair: TBA Meeting room 212 Modeling of a Business Aircraft using Research Aircraft Flight Simulator highest Level D of Certification Ruxandra Botez Range and endurance modelling of a multi-engine aircraft with one engine inoperative (OEI) Ye Naung Kyaw Kyaw 1450-1520 1520-1700 (25 min presentation) Structures & Materials II Chair: TBA Meeting Room 213 Transverse free vibration of rotating non-uniform EulerBernoulli beams using the Adomain modified decomposition method Desmond Adair A ground and operational vibration assessment of the RAAF PC-9/A airframe David Conser Active flow control methods on dynamic stall Joshua Yen Thoughts on accounting for the scatter seen in delamination growth Rhys Jones Computational Fluid Dynamic study of a Supersonic Ejector-Diffuser System Indukuri Lahari Sumanth Varma Afternoon tea – Level 2 Foyer Concurrent session 3 CGAP fatigue life calculation developments with improved elastoplastic constitutive modelling. Dylan Agius Aerospace design II Airworthiness & Regulations I HUMS II Helicopter Applications Chair: TBA Meeting room 218 HUMS III Life Cycle Management Chair: TBA Meeting room 215 CH-53 Rotor Loads Prediction Using the rotorwise Load Confluence Algorithm, Chance McColl Verification and Validation of Complex SystemsMethods, Tools and Challenges George Vachtsevanos Chair: TBA Meeting room 216 The impact of digital diffusion, adoption and adaptation on Small Unmanned Aerial Systems (SUAS) David Carr Chair: TBA Meeting room 217 Challenges to the airworthiness certification of unmanned aircraft systems Reece Clothier Linear matrix inequalitybased steering control law of variable speed control moment gyros for flexible spacecraft Shinya Kasai Design of a light, four-seat, zero-emissions aircraft John Page A generic model for quantification of risk posed by UAS ground impacts Vamsi Krishna Madasu Energy Harvesting, Wireless Fiber Optic Sensor (WiFOS™) Structural Health Monitor System for Helicopter Rotors Edgar Mendoza A case for good HUMS: The impact of exchange rate distributions on fleet availability and risk Nickolas Armstrong The changing face of Military Airworthiness Interactions Leon Purton Annual ADF cost of aircraft corrosion Lessons on designing against fatigue from multinational fatigue testing and service of the F/A-18 Hornet aircraft Loris Molent Kinetic Energy does not quantify the safety of personnel or materiel impacted by small UAS Javaan Chahl Investigation of a helicopter harsh landing based on signals from installed sensors Andrzej Leski Panel session TBA Aerodynamics III Structures & Materials III Aircraft operations I Airworthiness and Regulations II & System Support I Chair: TBA Chair: TBA Chair: TBA Chair: TBA Meeting room 212 Low Speed Stability Analysis of Hypersonic Cruise Vehicles Jonathan Jeyaratnam Meeting Room 213 Intermediate Failure Modes of Bolted Joints in Composite Materials Coel Gould Meeting room 216 Aerial Bushfire Quencher Cees Bil Meeting room 217 Engineer resilience in high reliability aerospace organisations Eric Wilson Experimental study on the impact of incorporating bioinspired leading edge tubercles on aerodynamics of the unmanned aerial vehicle wings Aswinraj An investigation of crack tip plastic zone size for metallic fatigue in highly stressed critical aerospace structures Autonomous communication between air traffic control and remotely piloted aircraft Luke Bouwmeester How must logistic frameworks adapt to support future unmanned systems Keirin Joyce HUMS IV Diagnostics/Condition Monitoring Chair: TBA Meeting room 218 HUMS V Land Chair: TBA Meeting room 215 Accelerated Testing of UH60 Viscous Bearings for Degraded Grease Fault Brian Dykas The issue for land HUMS is consistent data collection Keith Mowbray Estimating Bearing Fault Size using Vibration Analysis Wenyi Wang Condition Based Maintenance: Is Too Much of a Good Thing Bad? Guy Gallasch Tentative program 1900-2300 Rajendran Angelika Schuck Effect of the leading edge shape on the formation of asymmetric vortex flow over delta wing of varying sweep angles YongYing Zheng Development of Conductive coatings for Aircraft Skin Application Anand Khanna Business Plan: Viability of Using Moorabbin Airport as Destination for Scheduled Domestic Flight Asmamaw Negash Gebreegziabher Aerodynamic noise simulation of synthetic jet actuator application for stall delay Yendrew Yauwenas A Methodology of Integrating Convex Hull into Data Mining for Simulation of Helicopter Autorotation Yang Pei Experimental validation of ship-helicopter dynamic interface simulations using instrumented aircraft James Forrest Maintenance Requirements Determination (MRD) and Reliability Availability Maintainability (RAM) Disciplines in support of Army Aviation “From There to Here to Where?” Robert Crowe Is Engine Failure on the Runway at Takeoff the most limiting case? Bertrand Masson Vibration Comparison Between Conventional and Hybrid Angular Contact Bearings Kelsen LaBerge Generic Mobile Device deployment for Aerospace ground support equipmentHUMS Implementation Craig Watkins Development of Diagnosis Algorithms for HUMS Byung Hyun Ahn Models and Tools for the Cost/Benefit Analysis of Condition Based Maintenance Guy Gallasch Congress Banquet & Awards Tuesday 24 February 2015 0800-0900 0830-1015 1015- 1040 1040-1220 (25 min presentation) Registration opens Keynote Plenary – Meeting room 212/213 Keynote Address 2 Keynote Address 3 Morning tea – Level 2 Foyer Concurrent session 4 Propulsion I Structures & Materials IV Chair: TBA Chair: TBA Meeting room 212 Meeting Room 213 Extending range and Entrainment Defects in endurance estimates to Light Alloys battery powered electric William Griffiths aircraft Andrew Gong Assessment of Allowable Experimental Blade Damage Size for a determination of critical Blisk crack size for an aircraft Jianfu Hou bulkhead with oversized fastener holes Wyman Zhuang Airframe Surface Heating Multifunctional by a High Speed Micro composites exhibiting Jet Turbine Exhaust structural and thermal Plume management capabilities Yee Dah Kuo Everson Kandare Measurement of the NIR-reflective pigments to shock train speed in the improve the stability of isolator using wavelet airframe composites analysis Balwinder Kaur Zhi Chen HUMS Applications VI Aircraft operations II Chair: TBA Meeting room 216 Self-Organised Swarms; A technology for aerospace John Page Avionics & Mission Systems I Chair: TBA Meeting room 217 Closed-Loop Alternate Navigation Demonstration: Bilateral UAS Program Kent Rosser Recent Ergonomic Advances Deployed in Operational Air Traffic Control Human Machine Interfaces Mark O’Flynn GNSS Integrity Augmentation for Unmanned Aircraft Sense-andAvoid Robert Sabatini Leveraging of Experts Knowledge to Improve Diagnostic of Aircraft Engine T Sirizo Rabenoro Multi-Agent Collaborative Air Traffic Flow Management for Unmanned Aircraft Operations Trevor Kistan Exploring future display concepts to enhance the effectiveness of Army’s unmanned aerial system capability Low-Cost Sensors Data Fusion for Small and Medium Size RPAS Navigation and Guidance Subramanian Ramasamy A Standard for Filter Debris Analysis Andy Becker Comparison of numerical methods for the analysis of expansion-deflection nozzle Ananya Khare Analysis and Interpretation of Crack Propagation Signals Adrian Hood Chair: TBA Meeting room 218 HUMS Keynote 2 HeloTrackTM; Benefits and Challenges of Implementing the US Navy’s Newest Rotary Wing Dynamic Component Structural Life Tracking Patrick Dwyer Tentative program Peter Ryan 1220-1315 Lunch – Level 2 Foyer 1315-1455 (25 min presentation) Concurrent session 5 Structures & Materials V Aerospace design and Structures & materials III Chair: TBA Meeting Room 213 Effect of anodising treatments on equivalent crack size of the 7XXX aluminium alloy Alex Shekhter Chair: TBA Meeting room 216 Fault diagnosis of electrical discharge machining pulse generator using artificial neural networks Bo Hu Chair: TBA Meeting room 217 Equivalence of Magnetometer Calibrations and Soft Iron Magnetic Field Characterisation Andrew Ellis Numerical investigation An Aerospace Conformal of effects of turbulence Phased Array Slotted and reaction models on Waveguide Antenna combustion in scramjet Stiffened Structure nozzles with supersonic Thomas Baum after-burning Michael Candon Numerical analysis of a Development of an low angle linear aluminium alloy for expansion-deflection aerospace applications at nozzle in open wake higher temperatures conditions Subodh Kumar John Olsen Numerical investigation Effect of structural nonand optimisation of flow linearity on aeroelastic control effects of plasma response actuators for subsonic David Munk aerofoils in turbine applications Graham Bell Afternoon tea – Level 2 Foyer Concurrent session 6 An environment model for simulating small aircraft flight in the marine atmospheric boundary layer Jonathan Dansie Ground Obstacle Avoidance System for manned and unmanned aircraft Alessandro Gardi Implementation of Advanced Failure Analysis for an Improved Strength Prediction of FRC Parts Mukesh Bhasin An infrared vision system for UAV close formation flight Daniel Wilson Challenges in modelling fatigue crack growth under military transport and helicopter type spectra Weiping Hu A method for autonomous navigation of UAVs using landmarks Javaan Chahl Propulsion II Chair: TBA Meeting room 212 Environmental-energyharvesting technologies for unmanned air vehicles Jennifer Palmer 1455-1520 1520-1700 (25 min presentation) Aircraft Operations III and Airworthiness & Regulations III Chair: TBA Meeting room 212 The Development of a Mission Planning System for Unmanned Aircraft Operations in Windy Urban Environments Chung Sing Leung Avionics & Mission Systems II HUMS VII Structural Health Monitoring Chair: TBA Meeting room 218 A history of fatigue tracking the F/A-18 Hornet by the RAAF Lorrie Molent Determination of composite patch thickness on the accuracy of nondestructive testing of the repaired structure of PZL-130 ORLIK aircraft Michał Sałaciński Smart Pulse De-ice System for Composites with integral Ice Accretion and Structural Health Sensors Joseph Gerardi Prototype rotational energy harvester for structural health monitoring Scott Moss Chair: TBA Meeting room 215 Outcomes of the Corrosion Prognostic Health Management (CPHM) Capability and Technology Demonstrator (CTD), James Waldie Validation of an optical fibre based plate-wave mode conversion technique for damage detection in plates Cedrik Rosalie Placeholder-corrosion paper Evaluation of Modern Oil Condition Sensors for Lubrication Systems Paul Rawson Structures & Materials VI Aerodynamics IV and Propulsion III Avionics & Mission Systems III Chair: TBA Chair: TBA Chair: TBA Chair: TBA Chair: TBA Meeting room 217 Avionics-Based GNSS Integrity Augmentation for Remotely-Piloted Aircraft Systems Subramanian Ramasamy Meeting room 218 Meeting room 215 Meeting Room 213 Real-time risk management of aircraft fleet based on the probability of failure of aircraft structures Ribelito Torregosa Meeting room 216 Effect of wing flexibility in forward flight of tandem flapping wings Naidu Vishal HUMS IX Data Driven Applications HUMS VIII Sensor technologies I Leveraging HUMS for effective sustainment decisions Chris Stecki HUMS X Sensor technologies II An Introduction to Prognostic Fingerprint Technology John Baker Tentative program Exploiting natural resources to optimize flight paths for greener commercial flight operations Matthew Marino Critical Manufacturing and Future Trends in Aerospace Engine Materials Surya Kumar Singh Enhancing fatigue test outcomes through the use of bar-coded marker band load sequences Madeleine Burchill A CFD analysis of a passive flow control device on a sphere Nicholas Findanis Avionics-based GNSS Integrity Augmentation Performance in a jamming environment Roberto Sabatini A method through data overload: System Information Exploitation Paul Cree Investigation on Impact Damage Experimental Test and Repair Method of Composite Laminate for Aircraft Structural Design Hyunbum Park Mg Alloys for Seahawk Helicopters: Corrosion and its Mitigation Parama Banerjee Metal hydrides as additives for boron combustion Jianfei Xi Micro-Autopilot for Research and Development Kent Rosser Elements of a successful HUMS- lessons learnt from acquisition to sustainment Joanna Kappas Tests of Alternative Fuels in a Micro-Turbojet Engine Sean Spencer Communication, Navigation and Surveillance Integrity Performance Criteria for Safety-Critical Avionics and ATM Systems Design Roberto Sabatini Meeting room 218 1700-1725 A Rule Based Track Anomaly Detection Algorithm for Force Protection Sharada Boinepalli Congress Plenary Closing & Award Presentations 1900 – 2200 HUMS Conference dinner – Pier 35, Port Melbourne *Tentative program based on abstracts accepted; as at Thursday, 20 November 2014 Closing HUMS 2015 session Tentative-Moving Beyond Aircraft Health Monitoring Mythology: The journey towards obtaining tangible Life-Cycle Management ROI.
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