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