Monday, June 1, 2015 Fennia II, Scandic Marina Congress Center 07:30 Registration 8:30–8:45 Welcoming Address Aslak Siljander ICAF2013 Chairman Welcome Brig. Gen. Kari Renko Chief Engineer, Finnish Defence Forces Opening Address Anders Blom General Secretary of ICAF National Review – Australia Phil Jackson 8:45–9:00 9:00–9:15 9:15–10:00 10:00–10:30 Coffee Break & Exhibition Visit 10:30–12:00 Session 1 (Conference) Chairman: Steve Reed, UK National Review – The Netherlands Marcel Bos National Review – Japan Nobuo Takeda National Review – Israel Yuval Freed 10:30 11:00 11:30 12:00–13:00 Lunch Break and Exhibition visit 13:00–14:30 Session 2 (Conference) Chairman: Nobuo Takeda National Review – Sweden Hans Ansell National Review – Italy Luigi Lazzeri National Review – Poland Antoni Niepokólczycki 13:00 13:30 14:00 14:30–15:00 Coffee Break and Exhibition visit 15:00–17:00 Session 3 (Conference) Chairman: Claudio Dalle Donne National Review – Germany Claudio Dalle Donne National Review – France Thierry Ansart 15:00 15:45 18:00 ICAF Business Meeting (National Delegates only, meeting room “Lars” at Grand Marina Hotel) This meeting is for the ICAF National Delegates only. 20:00 ICAF National Delegates’ Dinner This event is for the ICAF National Delegates only. Preliminary ver2_030215 Tuesday, June 2, 2015 07:30 Registration 8:30–10:00 Session 4 (Conference) Chairman: Phil Jackson National Review – USA Ravi Chona National Review – Canada Nick Bellinger 8:30 9:15 10:00–10:30 Coffee Break and Exhibition visit 10:30–11:45 Session 5 (Conference) Chairman: Ravi Chona National Review – Switzerland Michel Guillaume National Review – UK Stephen Reed 10:30 11:00 11:45–13:00 Lunch Break and Exhibition visit 13:00–16:00 Session 6 Chairman: Anders Blom National Review – Brazil Carlos E. Chaves National Review – China N.N. (TBD) National Review – Russia N.N. (TBD) National Review – Finland Aslak Siljander 13:00 13:45 14:30 15:15 Preliminary Fennia II, Scandic Marina Congress Center ver2_030215 Wednesday, June 3, 2015 Fennia II, Scandic Marina Congress Center 07:30 Registration 8:00–9:30 Session 1 (Symposium) – Plantema Lecture Chairman: Aslak Siljander, Finland Welcoming note Jukka Holkeri Chief Strategy Officer, Patria 8:05 8:15 Introduction Anders Blom General Secretary of ICAF 8:30 Plantema Memorial Lecture Structural Integrity – the unfinished business Jerzy Komorowski General Manager (Aerospace Portfolio), National Research Council Canada and former Canadian ICAF delegate Presentation of the Plantema Medal 9:15 st 9:30–10:00 Coffee Break and Exhibition & Poster viewing – The 1 poster set 10:00–12:00 Session 2 (Symposium) – Advanced analytical, numerical and experimental methods Chairman: Luigi Lazzeri, Italy Fatigue prediction of additive manufactured Ti-6Al-4V for aerospace: Effect of defects, surface roughness Daniel Greitemeier Airbus Group Innovations, Germany Validation of the USAF characteristic K approach for naturally occurring small cracks under a combat aircraft load spectrum Dinaz Tamboli Monash University, Australia Is the world ready for HOLSIP? 1 2 3 Paul N. Clark , Nicholas Bellinger , David W. Hoeppner 1 2 3 Southwest Research Institute, USA; National Research Council, Canada; University of Utah, USA How proper similitude principles could have improved our understanding about fatigue damage growth René Alderliesten Delft University of Technology, the Netherlands 10:00 10:30 11:00 11:30 st 12:00–13:00 Lunch Break and Exhibition & Poster viewing – The 1 poster set 13:00–14:30 Session 3 (Symposium) – Widespread fatigue damage Chairman: Hans Ansell, Sweden WFD evaluation of riveted lap joint 1 2 1 2 2 Takao Okada , Min Liao , Shigeru Machida , Gang Li , Guillaume Renaud 1 2 Japan Aerospace Exploration Agency (JAXA), Japan; National Research Council Canada (NRC), Canada A risk analysis based methodology for widespread fatigue damage evaluation Yuval Freed, Dvir Elmalich, Abraham Brot, Yael Buimovich and Carmel Matias Israel Aerospace Industries, Israel Curved panel fatigue test for MRJ-200 pressurized cabin structure 1 1 1 2 2 Kaoru Tsukigase , Toshiyasu Fukuoka , Keisuke Kumagai , Toshio Nakamura , Shunsuke Taba 1 2 Mitsubishi Aircraft Corporation, Mitsubishi Heavy Industries, LTD., Japan 13:00 13:30 14:00 Preliminary ver2_030215 Wednesday, June 3, 2015 Fennia II, Scandic Marina Congress Center st 14:30–15:00 Coffee Break, Exhibition & Poster viewing – The 1 poster set 15:00–16:00 Session 4 (Symposium) – Engine Integrity Chairman: Nick Bellinger, Canada Effect of shot peening on low cycle fatigue behavior of Ti-6Al-4V 1 1 2 2 Hiroshi Nakamura , Tatsuhito Honda , Joris Prou , Mitsuyoshi Tsunori 1 2 IHI Corporation, Aero-Engine & Space Operations, IHI Corporation, Reserch labolatory, Japan Multi-scale approach for the analysis of the stress gradient effect in fretting-fatigue 1 1 2 2 2 Claudio Montebello , Sylvie Pommier , Karim Demmou , Julien Leroux , Jean Meriaux 1 2 LMT-Cachan (ENS Cachan/CNRS), Snecma Villaroche, France 15:00 15:30 16:00–17:30 16:00 16:30 17:00 18:30–20:00 Preliminary Session 5 (Symposium) – Adhesively Bonded Repairs / Reinforcements Chairman: Steve Reed, UK Evaluation of adhesively bonded repairs to fuselage structure subjected to environmental conditions 1 2 3 4 5 5 John G. Bakuckas, Jr. , Bin Lei , Yongzhe Tian , Ian Y. Won , Kelly Greene , Carlyn Brewer , 6 6 Jonathan Awerbuch , Tein Min Tan 1 2 3 FAA William J. Hughes Technical Center, FAA-Drexel Fellow, FAA Technical Center, Hiasun Inc., 4 5 FAA Technical Center, FAA Transport Airplane Directorate, Boeing Research & Technology, 6 Drexel University, USA Fatigue strength of adhesively bonded joints of CFRP with laser surface treatment 1 1 2 3 4 Tomohiro Yokozeki , Keigo Sato , Masaru Ishibashi , Hideyasu Shamoto ,Yutaka Iwahori 1 2 3 4 University of Tokyo, GSI Creos Corporation, Laserx Co., Japan Aerospace Exploration Agency, Japan Full-scale fatigue testing of a boron-epoxy bonded doubler for the Finnish Air Force F/A-18 Hornet centre fuselage 1 2 2 Geoff Swanton , Mika Keinonen , Janne Linna 1 2 Defence Science and Technology Organisation, Australia, Patria Aviation, Finland Symposium Cocktail Reception The Old Town Hall, Pohjoisesplanadi 11–13 Hosted by the City of Helsinki Dress code: Smart casual or come as you are Welcoming address by City of Helsinki representative Welcoming address by Jouko Suokas, Executive Vice President, VTT ver2_030215 Thursday, June 4, 2015 Fennia II, Scandic Marina Congress Center 07:30 Registration 8:15–9:45 Session 6 (Symposium) – Advanced analytical, numerical and experimental methods Chairman: Ravinder Chona, USA An algorithm for the prediction of very high cycle fatigue Life Andrew Whitelaw, RJ Amos, MA Hussain MBDA – UK Limited, United Kingdom Improving the prediction of short crack growth fatigue in 7XXX aluminum alloys 1 2 1 Simon Barter , Michael Jones , Madeleine Burchill 1 2 Defence Science and Technology Organisation, Fortburn, Australia Stress analyses of bolted joints containing part-through cracks and exhibiting secondary bending Hans Ansell, Zlatan Kapidžić, Lars Djärv Saab AB, Sweden 8:15 8:45 9:15 nd 9:45–10:15 Coffee Break, Exhibition & Poster viewing – The 2 poster set 10:15–11:15 Session 7 (Symposium) – Residual Stress Engineering Chairman: Antoni Niepokólczycki, Poland Predicting fatigue crack growth emanating from cold-expanded holes 1 2 3 2 2 Luigi Lazzeri , Domenico Furfari , Qiang Fu , Anja Wetzel , Mauro Bruno Biasizzo , David Osman 2 Busse 1 2 3 Pisa University, Italy; Airbus Operations GmbH, Germany; Airbus Operations Ltd, United Kingdom Validation of new experimental and analytical tools to address residual stress effects accurately in the design cycle: Material characterization and design analysis validation 1 2 Mark A. James , R. Craig McClung 1 2 Alcoa Technical Center, USA; Southwest Research Institute, USA 10:15 10:45 11:15–12:15 11:15 11:45 12:15–13:15 13:15–14:15 13:15 13:45 Preliminary Session 8 (Symposium) – Composite materials development of innovative structural concepts Chairman: Antoni Niepokólczycki, Poland Fatigue and damage tolerance assessment of 3-D reinforced CFRP bonded joints 1 2 2 Chiara Bisagni , Domenico Furfari , Marco Pacchione 1 2 Politecnico di Milano, Italy; Airbus Operations GmbH, Germany Philosophy of multiple-site damage analysis for fibre metal laminate structures Wandong Wang, Calvin Rans, Rene Alderliesten, Rinze Benedictus Faculty of Aerospace Engineering, Delft University of Technology, the Netherlands nd Lunch Break, Exhibition & Poster viewing – The 2 poster set Session 9 (Symposium) – Airworthiness regulations and substantiation methodology development Chairman: Thierry Ansart, France Damage tolerance approach on recurrent damages of Lynx helicopters Etienne Deshaies, Chloé Kinzelin, Pierre Madelpech DGA Aeronautical Systems, France Structural durability and damage tolerance in the next century of commercial aviation Steven Chisholm, Antonio Rufin, Brandon Chapman, Quentin Benson The Boeing Company, USA ver2_030215 Thursday, June 4, 2015 14:15–15:15 14:15 14:45 Fennia II, Scandic Marina Congress Center Session 10 (Symposium) – Fleet Monitoring Chairman: Thierry Ansart, France The A400M usage monitoring function Alexis Falga, Alain Santgerma, Jean-Pascal Kleinermann Airbus Operations SAS, France The use of micro electro-mechanical systems to characterise the structural usage of a multi-role military aircraft Robin Kamiya, Michael Duffield QinetiQ, United Kingdom nd 15:15–15:45 Coffee Break, Exhibition & Poster viewing – The 2 poster set 15:45–16:45 Session 11 (Symposium) – Non-destructive inspection (NDI) development and implementation Chairman: Phil Jackson, Australia Reliability based approach for assessing different SHM and load monitoring systems under load and environmental conditions Shashank Pant, David Backman, Tom Benak, Marc Genest National Research Council, Canada Probing the future: Better F-16 inspections using conformal Eddy Current inspection tools 1 2 3 1 Kimberli Jones , John Brausch , Ward Fong , Bryce Harris 1 2 3 United States Air Force (F-16 ASIP), United States Air Force Research Laboratory, United States Air Force (Ogden ALC), USA 15:45 16:15 16:45–18:45 16:45 17:15 17:45 20:00–23:30 Preliminary Session 12 (Symposium) – Full Scale Fatigue Tests and Management of Aging Fleets Chairman: Michel Guillaume, Switzerland A350 XWB EW Test - Combined static and fatigue testing of composite aircraft structures within one test set up 1 1 2 Fin Schorr , Michael Stodt , Timo Plate 1 2 IABG mbH, Airbus Operations GmbH, Germany Advanced life assessment of the lead crack configuration of the RNLAF F-16 wing damage enhancement test Frank Grooteman, Marcel Bos National Aerospace Laboratory NLR, the Netherlands Practical Experience of neural network based fatigue life monitoring Jarkko Tikka, Tuomo Salonen Patria Aviation, Finland Symposium Gala Dinner Restaurant Saaristo (Klippan) Next to Statue of Peace, Ehrenströmintie 10, South Harbour ver2_030215 Friday, June 5, 2015 Fennia II, Scandic Marina Congress Center 07:30 Registration 8:15–9:00 8:15 Session 13 (Symposium) – Schijve Award & Lecture Chairman: Marcel Bos, the Netherlands Announcement of the winner 8:30 Jaap Schijve Award Lecture 9:00–10:00 9:00 9:30 10:00–10:30 10:30–12:00 10:30 11:00 11:30 Session 14 (Symposium) – Advanced analytical, numerical and experimental methods Chairman: Marcel Bos, the Netherlands Composite door pressure fatigue test Frank Wießner, Martin Semsch IMA Materialforschung und Anwendungstechnik GmbH, Germany Experimental determination of the crack tip stress intensity factor in integrally stiffened panels Caio Magno de Assunção, Carlos Eduardo Chaves EMBRAER S/A, Brazil rd Coffee Break, Exhibition & Poster viewing – The 3 poster set Session 15 (Symposium) – Airworthiness regulations and substantiation methodology development Chairman: Yuval Freed, Israel Hawk, the 21st century trainer Robert Young BAE Systems, United Kingdom F-35 full scale durability modeling and test Dale L. Ball, Philip C. Gross, Robert J. Burt Lockheed Martin Aeronautics Co., USA Structural integrity assessment of Gripen NG aircraft Hans Ansell Saab AB, Sweden rd 12:00–13:00 Lunch Break, Poster viewing – The 3 poster set 13:00–14:00 Session 16 (Symposium) – Digital Twins Chairman: Claudio Dalle Donne, Germany An assessment of a virtual full scale fatigue test methodology using full scale fatigue test data Chris Wallbrink, Michael Opie, Xiaobo Yu Defence Science and Technology Organisation, Australia Advances in computational nondestructive testing 1 2 David Forsyth , John Aldrin 1 2 TRI/Austin Inc., Computational Tools, USA 13:00 13:30 Preliminary ver2_030215 Friday, June 5, 2015 14:00–15:00 14:00 14:30 Fennia II, Scandic Marina Congress Center Session 17 (Symposium) – Probabilistic modelling and risk analysis of structural integrity Chairman: Claudio Dalle Donne, Germany Application of quantitative risk analysis in support of continuing airworthiness management Min Liao, Guillaume Renaud, Yan Bombardier Aerospace Portfolio, National Research Council Canada (NRC), Canada Probabilistic approach to the inspection interval determination in a multi-site damage susceptible structure Javier Segurado, Pablo Caffyn, Jaime Garcia, Blanca de Nicolás, Jose Ignacio Armijo, Daniel Iñesta Airbus Defence & Space, Spain rd 15:00–15:30 Coffee Break, Poster viewing – The 3 poster set 15:30–17:00 Session 18 (Symposium) – Corrosion and Environmental Control (Management of Aging Fleets) Chairman: Nobuo Takeda, Japan Evaluation of the structural impact of pitting corrosion damage on a lower wing skin 1 1 2 2 Andreas Uebersax , Raphael Zehnder , Guillaume Renaud , Min Liao 1 2 RUAG Aviation, Switzerland, National Research Council, Canada Simulation of corrosion damage, stress concentration, and fatigue crack growth Sharon Mellings, John Baynham, Andres Peratta CM BEASY, United Kingdom The decoupling of corrosion and fatigue for aircraft service life management 1 2 2 Russell Wanhill , Simon Barter , Loris Molent 1 2 National Aerospace Laboratory NLR, the Netherlands, Defence Science and Technology Organisation, Australia 15:30 16:00 16:30 17:00–17:15 Preliminary Symposium closure, pre-announcement of ICAF 2017 Aslak Siljander, Finland Pre-announcement of ICAF 2017 (ICAF 2017 host nation’s National Delegate) Anders Blom, General Secretary of ICAF ver2_030215 Poster sets for Wednesday to Friday Poster set #1 Advanced analytical, numerical and experimental methods Challenges and progress in modelling fatigue crack growth under transport aircraft and helicopter type spectra Weiping Hu, Beau Krieg, Phil Jackson, Matt McCoy, Kai Maxfield, Rob Ogden Defence Science and Technology Organisation, Australia Closed form equations of stress intensity factors for angle shaped cross-section with through crack Toshimi Taki Kawasaki Heavy Industries, Ltd., Japan The influence of the stress state on the power law exponent of the fatigue crack growth rate Emiel Amsterdam, Frank Grooteman National Aerospace Laboratory (NLR), the Netherlands Effective structural health monitoring system for 3D printed components 1 1 2 3 1 1 M. Hinderdael , D. De Baere , M. Strantza , R. Vafadari , W. Devesse , P. Guillaume 1 2 Department of Mechanical Engineering, Vrije Universiteit Brussel, Belgium; Department of Mechanics of 3 Materials and Constructions, Vrije Universiteit Brussel, Belgium; Department of Materials Science and Engineering, Ghent University, Belgium PGD-virtual charts for structural design: application to geometrical parameters 1,2 1 1 2 2 Amaury Courard , David Néron , Pierre Ladevèze , Alain Bergerot , Ludovic Ballere 1 2 LMT Cachan (ENS Cachan/CNRS/Université Paris-Saclay), France; AIRBUS Defence and Space, France Reducing weight by bionic shape optimization of triangular levers Dort Daandels, Sarah Payros, Mark Knuebel, Alexander Bruns, Olivier Seack Airbus Operations GmbH, Germany An operational load related method for fatigue tests on aircraft components Martin Semsch, Andreas Schelenz, Alexander Hamann, Silvio Nebel IMA Materialforschung und Anwendungstechnik GmbH Dresden, Germany Development of analysis and test methods for lightning current flow on composite fuel tank structure Hiroshi Fujisawa, Takayuki Nishi, Yasunori Sato Fuji Heavy Industries LTD., Japan Non-stationary models for predicting strain on aircraft landing gear from flight data measurements 1 2 2 1 1 Geoffrey Holmes , Valerijan Cokonaj , Paul Southern , Keith Worden , Elizabeth Cross , 1 2 The University of Sheffield, United Kingdom; Messier-Bugatti-Dowty, United Kingdom Effect of periodicity and reverse yielding on cyclic loading of notched specimens 1 2 Floyd Caiado , S. Keshavanarayana 1 2 Textron Aviation, USA; Wichita State University, USA Cold spot welding in riveting joint 1 1 2 Wojciech Wronicz , Jerzy Kaniowski , Krystyna Pietrzak 1 2 Institute of Aviation, Poland; Motor Transport Institute, Poland Strength, fatigue and crack growth resistance of Al-alloys that are applied in current transport airplanes wing and fuselage skin Boris Nesterenko, Grigory Nesterenko, Aleksandr Kulemin Central Aerohydrodynamic Institute (TsAGI), Russia Widespread Fatigue Damage Analytical modeling of mechanical joint for new monitoring method Shigeru Machida, Takao Okada Japan Aerospace Exploration Agency (JAXA), Tokyo, Japan Fatigue life assessment of PZL-130 Orlik structure – final analyses and results Andrzej Leski, Marcin Kurdelski, Piotr Reymer, Krzysztof Dragan, Michal Salacinski Air Force Institute of Technology, Poland Preliminary ver2_030215 Peridynamics for crack initiation and propagation under cyclic loading 1 2 3 Erdogan Madenci , Arash Zamani , Nam Phan 1 2 3 The University of Arizona, USA; Global Engineering Research and Technologies, USA; Naval Air Systems Command (NAVAIR), USA Engine Integrity On the competition between stress gradient effect and size effect in fretting fatigue 1,2 & 3 1 2 3 Barbara Ferry , Sylvie Pommier , José Alexander Araujo , Karim Demmou 1 2 LMT-Cachan, ENS Cachan, France; Universidade de Brasilia, Departamento de Engenharia Mecânica, Brasil; 3 SNECMA, groupe SAFRAN, France Shot peening residual stress evaluation from 3D finite element simulation 1 1 2 Joris Prou , Mitsuyoshi Tsunori and Hiroshi Nakamura 1 2 IHI Corporation, Structural Strength Department, Japan; IHI Corporation, Engine Technology Department, Japan Development of composite structural guide vane for the new turbo fan engine 1 1 1 1 1 1 Takaomi Inada , Hiroyuki Yagi , Hideo Morita , Rintarou Kajiwara , Takehisa Yamada , Tsutomu Murakami , 1 1 1 2 Koji Miyazawa , Takehiko Uchiyama , Katsuyoshi, Moriya , Shinichi Tanaka 1 2 IHI Corporation, Japan; IHI Aerospace Co., Ltd., Japan Adhesively Bonded Repairs / Reinforcements Validation of a UAV composite wing spar repair using an embedded optical fiber Rayleigh back-scattering distributed strain sensing 1 2 2 3 3 2 2 1 A. Bergman , U. Ben-Simon , A. Schwartzberg , N.Y. Shemesh , B. Glam , J. Burvin , I. Kressel , M.Tur 1 2 School of Electrical Engineering, Tel-Aviv University, Tel-Aviv Israel; IAI Engineering Division Ben Gurion 3 International Airport 70100 Israel; IAF Structure Branch Application of distributed fiber optic strain sensors for local indentation/impact damage detection in foam core composite sandwich structures Juho Siivola, Shu Minakuchi, Nobuo Takeda The University of Tokyo, Japan Back to programme Poster set #2 Residual Stress Engineering Laser shock peening as surface technology to extend fatigue life in metallic airframe structures NOT CONFIRMED 1 1 2 2 2 Domenico Furfari , Nikolaus Ohrloff , Elke Hombergsmeier , Ulrike C. Heckenberger , Vitus Holzinger 1 2 Airbus Operations GmbH, Germany; Airbus Group Innovations, Germany Effect of LSP generated residual stresses on fatigue crack propagation in thin panels 1 1 2 2 3 Enrico Troiani , Sara Taddia , Ivan Meneghin , Gianluca Molinari , Claudia Polese 1 2 3 MasterLab University of Bologna, Italy; Sii Deutschland GmbH, Germany; University of Witwatersrand, Johannesburg, South Africa Composite materials development of innovative structural concepts Experimental study on partial composite wing structure 1 2 2 3 3 Hikaru Hoshi , Takao Okada , Yutaka Iwahori , Satoshi Morooka , Naoyuki Watanabe 1 2 Institute of Aeronautical Technology, Japan Aerospace Exploration Agency, Japan; Institute of Aeronautical 3 Technology, Japan Aerospace Exploration Agency, Japan; Department of Aerospace Engineering, Tokyo Metropolitan University, Japan Fatigue bearing failure of CFRP composite in biaxially loaded bolted joints at elevated temperature Zlatan Kapidžić, Hans Ansell Saab AB, Sweden Damage tolerance assessment of edge impacts in CFRP structures 1,3 1 1 1 2 2 Vjola Ristori , Enrico Troiani , Maria Pia Falaschetti , Marco Montemurro , André Baeten , Goran Ivetic , 3 Gianluca Molinari 1 2 3 University of Bologna, Forlì, Italy; Augsburg University of Applied Sciences, Germany; Sii Deutschland GmbH, Germany Preliminary ver2_030215 Evaluation of transverse crack initiation in cross-ply and quasi-isotropic CFRP laminates under fatigue loading 1 2 1 Atsushi Hosoi , Yuzo Fujita , Hiroyuki Kawada 1 2 Departement of applied mechanics and aerospace engineering, Waseda university, Japan; Composite Materials Research Laboratories, Toray Industries, Inc., Japan Fleet Monitoring Data reduction of flight test and FEM data sets and application to fatigue load spectra development Nazim Ould Brahim, Maxime Lapalme Bell Helicopter Textron Canada Limited, Canada In-slight structural health monitoring system for high altitude long endurance unmanned air vehicle 1 1 2 3 4 4 4 2 3 I. Kressel , J. Balter , N. Mashiach , I. Sovran , O. Shapira , N.Y. Shemesh , B. Glam , A. Dvorjetski , M. Tur 1 2 3 IAI Engineering Division, Ben Gurion International Airport Israel; IAF UAVs Branch, Tel-Aviv Israel; School of 4 Electrical Engineering, Tel-Aviv University, Tel-Aviv Israel; IAF Aircraft Structure Branch, Tel-Aviv Israel Low-cost fixed-wing aircraft structural usage validation Steve Reed Defence Science and Technology Laboratory, United Kingdom The fatigue damage spectrum: Explained 1 2 Rob Plaskitt , Andrew Halfpenny 1 2 UK Application Engineering, HBM-nCode, United Kingdom; Chief Technologist, HBM-nCode, United Kingdom Review of computational methods for payload life prediction RJ Amos, A Whitelaw, MA Hussain MBDA – UK Limited, Six Hills Way, Stevenage, Hertfordshire, SG1 2DA, United Kingdom Challenges and proposed methodologies for structural health and usage monitoring systems (SHUMS) in the domain of airborne complex weapons 1 1 2 C Lomax , A Whitelaw , A Groves 1 2 MBDA (UK) Ltd, Six Hills Way, Stevenage, Hertfordshire, United Kingdom; Dstl, Porton Down, Salisbury, Wiltshire, United Kingdom MH-60 fleet usage and fatigue life monitoring using regime recognition 1 2 Suresh Moon , Daniel Liebschutz 1 2 Chief Engineer Air Vehicle Engineering, Engility, USA; Team Lead Engineer, Rotary Wing Structures, NAVAIR, USA Flight condition recognition and independent flight severity monitoring for the management of helicopter fleets Brian Perrett HeliSAC Limited, United Kingdom Non-destructive inspection (NDI) development and implementation Novel thermographic inspection method to detect the moisture in early stage of the water ingress and a procedure to remove the moisture from the composite structure 1 2 Eetta Saarimäki , Yrjö Laatikainen 1 2 VTT Technical Research Centre of Finland Ltd, Finland; Patria Aviation Oy, Finland Integrated health monitoring of the composite structures based on PZT sensors Krzysztof Dragan, Michał Dziendzikowski, Artur Kurnyta, Andrzej Leski Air Force Institute of Technology, Airworthiness Division Warsaw, Poland Sensor location studies for damage detection in aerospace structures using 3D scanning laser vibrometery R. Marks, A. Clarke, K. Holford, C. Featherston, L. Kawashita, R. Pullin Cardiff School of Engineering, Cardiff University, UK Long-term durability of adhesively bonded composite joints under static and fatigue loading 1 1 2 3 1 Chun Li , Zhong Yi Wan , Gabriel LaPlante , Calvin Rans and Gang Li 1 2 National Research Council Canada, Aerospace, Ottawa, Canada; Department of Mechanical Engineering, 3 Université de Moncton, Moncton, Canada; Faculty of Aerospace Engineering, Delft University of Technology, The Netherlands Preliminary ver2_030215 Design of health and usage monitoring systems based on optical fibers for composite wing spars 1 1 1 2 3 1 Alessandro Airoldi , Paolo Bettini , Paolo Belotti , Theodoros Loutas , Christos Koimtzoglou , Giuseppe Sala 1 2 Dept. of Aerospace Science and Technology, Politecnico di Milano, Italy; Dept. of Mechanical Engineering 3 and Aeronautics, University of Patras, Greece; Integrated Aerospace Science Corporation (INASCO), Athens, Greece Full Scale Fatigue Tests and Management of Aging Fleets Hornet outer wing StAtic testing (HOWSAT) program for RAAF classic Hornet service life management 1 1 1 2 2 2 Ben Main , Matt Gordon , Liam Weibler , Wayne Foster , Simon Barter and Loris Molent 1 Directorate General Technical Airworthiness RAAF Williams, Australia 2 Aerospace Division, Defence Science and Technology Organisation, Australia Full scale fatigue testing of two T-38 wings 1 2 3 David Wieland , Jon Cutshall , Michael Blinn 1 2 3 Southwest Research Institute, USA; Southwest Research Institute, USA; AFLCMC/WLDEJ United States Air Force, USA Back to programme Poster set #3 Airworthiness regulations and substantiation methodology development Random vibrations fatigue analysis and tests Etienne Deshaies, Jérémy Bernadou, Pierre Madelpech DGA Aeronautical Systems, France Tackling the characterization of H-60 airframe in-flight dynamic response and fatigue loading using small scale high performance computing John Vine, Luther Krake, Phil Jackson Defence Science and Technology Organisation (DSTO), Australia Value of metallurgical analysis in safety investigations Ismo Aaltonen Safety Investigation Authority, Finland Fatigue crack growth prediction using PREFFAS model Bertrand Journet Airbus Group Innovations, France An amphibian and the concept of its derivative model for firefighting application Hideyuki Mochida, Katsuo Tanaka, Atsuhiko Fujitani, Yushi Goda, Masatoshi Tsujii ShinMaywa Industries, Ltd., Japan Digital Twins Hardware-in-the-loop integrated fatigue test simulation (HiLiFTS) Albert K. Wong Defence Science & Technology Organisation (DSTO), Australia Probabilistic modelling and risk analysis of structural integrity Crack growth variability and its effect on assessment of probability of fracture of aircraft structures Ribelito Torregosa, Weiping Hu Aerospace Division, Defence Science and Technology Organisation, Australia Predicting multi-site fatigue in fuselage lap joints: Development of predictive model from experimental observations 1 2 Sandeep Shah , James Greer, Jr. 1 2 Sabreliner Aviation LLC, USA; United States Air Force Academy, USA Preliminary ver2_030215 Corrosion and Environmental Control (Management of Aging Fleets) Fatigue crack growth from environmentally induced damage in 7075 alloy 1 1 1 1 2 3 Michael Lo , Rhys Jones , Daren Peng , Daren Peng , Adam Bowler , Dustin Edwards 1 2 Department of Mechanical and Aerospace Engineering, Monash University, Australia; Maritime Systems 3 Project Office, RAAF Base Edinburgh, Australia; Airbus Australasia Pacific, Australia Stress-corrosion cracking and its prevention in space applications 1 1 1 Andreas Tesch , Adrian J. Graham , Tommaso Ghidini 1 ESA, European Space Agency, Materials Technology Section, The Netherlands Standardized methodology for the Investigation of corrosion fatigue nucleation and propagation Sarah E. Galyon Dorman, Divakar Mantha, Matthew J. Hammond, Scott A. Fawaz SAFE Inc, Center for Aircraft Structural Life Extension, United States Back to programme Preliminary ver2_030215
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