Elsevier reserves the right to change the program prior to the conference.
Sunday 14 September 2008 |
14.00 |
Conference registration and poster set-up |
17.00 |
Drinks reception and opening poster session
(General poster viewing – all themes) |
18.00 |
Dinner |
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Monday 15 September 2008 |
07.30 |
Registration |
08.15 |
Introduction and welcome
Conference co-chairs |
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Session 1: Design concepts - I |
08.30 |
KEYNOTE
Fleet management issues and technology needs
P. Hoffman*; NAVAIR, USA |
09.10 |
Spectrum editing effects on lifing of aircraft structural components
N. Iyyer*¹, R. Merrill¹, S. Sarkar¹, N. Phan²; ¹Technical Data Analysis, Inc., USA, ²U.S.Naval Air
Systems Command, USA |
09.40 |
Prognosis for structural health prognosis using mechanistic multistage fatigue model
Y. Xue*¹, J.B. Jordon¹, M.F. Horstemeyer¹, D.L. McDowell², J. Newman¹; ¹Mississippi State University, USA, ²Georgia Institute of Technology, USA |
10.10 |
Short crack model development for primary airframe material
M. Liao*, T. Benak, et al; Institute for Aerospace Research, Canada |
10.40 |
Refreshments |
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Session 2: Design concepts - II |
11.10 |
Generation and analysis of FCG data using a single specimen and Kmax - DK testing matrix
D. Kujawski*, P.C. Sree; Western Michigan University, USA |
11.40 |
Incorporating residual stress into the crack growth design practice using ACR concepts
M. James*¹, D. Ball², J. Brockenbrough¹, R. Bucci¹, K. Donald³; ¹Alcoa, USA, ²Lockheed, USA, ³Fracture Technology Associates, USA |
12.10 |
CDM approach applied to fatigue crack propagation on aeronautical metallic alloys
H.F. Hamon*¹, H.G. Henaff¹, H.D. Halm¹, B.T. Billaudeau², B.S. Bezamat²; ¹Physical and Mechanical
Laboratory of Materials, France, ²AIRBUS, France |
12.40 |
Poster viewing
(Poster session 1 –Theoretical approaches, modeling and life prediction
methodologies) |
13:10 |
Lunch |
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Session 3: Crack initiation criteria |
14.00 |
Analysis of fatigue crack nucleation using the unified damage approach
K. Sadananda*¹, G. Glinka², A.K. Vasudevan³; ¹Technical Data Analysis, Inc, USA, ²University of Waterloo, Canada, ³Office of Naval Research, USA |
14.30 |
Development of a dual crack nucleation – crack propagation approach to formalize the
fretting fatigue damages
S. Fouvry*, K. Kubiak; Ecole Centrale de Lyon, France |
15.00 |
Crack initiation and crack path growth under mutiaxial fatigue loading for structural steels
L. Reis, M. de Freitas*, B. Li; Instituto Superior Técnico, Portugal |
15.30 |
On the fatigue behavior of bifurcated cracks under near-threshold conditions
A.C.O. Miranda, M.A. Meggiolaro*, J.T.P. Castro, L.F. Martha; Pontifical Catholic University of Rio de Janeiro, Brazil |
16.00 |
Refreshments |
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Session 4: Crack tip plasticity |
16.30 |
Insights into mechanical mechanisms derived from synchrotron based fatigue crack strain
mapping
M. Croft*¹,², V. Shukla¹, N. Jisrawi³, Z. Zhong², R. Sadangi¹, R. Holtz¹, P.Pao4 et al; ¹Rutgers, USA, ²NSLS, USA, ³Sharjah, United Arab Emirates, 4NRL, USA |
17.00 |
On the size and shape of plastic zones ahead of crack tips
H.Z. Rodríguez, J.T.P. Castro*, M.A. Meggiolaro; Pontifical Catholic University of Rio de Janeiro, Brazil |
17.30 |
Elastic-plastic stress-strain analysis ahead of a growing fatigue crack
A.B. Buczynski¹, G.G. Glinka*²; ¹Warsaw University of Technology, Poland, ²University of Waterloo, Canada |
18.00 |
Close of Day 1 |
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Tuesday 16 September 2008 |
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Session 5: Fatigue / Environment – Al alloys |
08.30 |
KEYNOTE
Environmental effects in prognosis of airframe aluminum alloys
R.P. Gangloff*¹, J.R. Burns², et al; ¹University of Virginia, USA, ²Air Force Research Laboratory, USA |
09.10 |
Effect of environment on fatigue crack growth in ultra-fine grain Al-7.5Mg
P.S. Pao*¹, A.K. Vasudevan², R.L. Holtz¹, H.N. Jones¹, C.R. Feng¹; ¹Naval Research Laboratory, USA, ²Office of Naval Research, USA |
09.40 |
Influence of frequency and loading waveform on the corrosion fatigue crack propagation
behaviour of the aluminium alloy 2024-T351
F. Menan*, G. Henaff; LMPM-ENSMA, France |
10.10 |
The effects of aqueous environment on fatigue crack growth in 7075-T6 aluminum alloy
A.K. Vasudevan*¹, P. Pao², et al; ¹Office of Naval Research, USA, ²Naval Research Laboratory, USA |
10.40 |
Refreshments |
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Session 6: Fatigue / Environment – Ni alloys |
11.10 |
Plain and notched fatigue in nickel single crystal alloys
W.J. Evans*¹, M.T. Whittaker¹, R. Lancaster¹, A. Steele¹, N. Jones²; ¹Swansea University, UK, ²Rolls-Royce plc, UK |
11.40 |
Environment and time dependent effects on the fatigue response of an advanced nickel
based superalloy
M.R. Bache*¹, J.P. Jones¹, M.C. Hardy², G.L. Drew²; ¹Swansea University, UK, ²Rolls-Royce, UK |
12.10 |
Oxidation assisted fatigue crack growth under complex non-isothermal loading conditions
in a nickel base superalloy. Experiments and modeling
S.N. Pommier*, J.A. Ruiz-Sabariego; LMT-Cachan, France |
12.40 |
Poster viewing
(Poster session 2 –Extreme environments, residual stress effects, and sprectrum
loading) |
13:10 |
Lunch |
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Session 7: Multiaxial fatigue |
14.00 |
KEYNOTE
Multiaxial fatigue damage
D. Socie; University of Illinois, USA |
14.40 |
An experimental evaluation of critical plane multiaxial fatigue criteria
Y. Jiang*; University of Nevada, USA |
15.10 |
History effect in fatigue under mixed mode loading conditions
P.Y. Decreuse*, S.N. Pommier, L. Gentot, S. Pattofatto; LMT-Cachan, France |
15.40 |
Fatigue damage accumulation in Ti-6Al-4V under simulated multiaxial mission spectra
A.R. Kallmeyer*¹, S.K. Suman¹, E.T. Goodin¹, P. Kurath²; ¹North Dakota State University, USA,
²University of Illinois, USA |
16.10 |
Refreshments |
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Session 8: –Internal stress and pre-strain |
16.40 |
Mean stress relaxation and strain-life fatigue in high strength aluminum alloys
A. Arcari, R. De Vita, N.E. Dowling*; Virginia Tech, USA |
17.10 |
Effect of prestrain on the fatigue properties of Ti-834
W.J. Evans, M.T. Whittaker*; Swansea University, UK |
17.40 |
Notch fatigue resistance of shot peened high strength aluminium alloys: The role of
residual stress relaxation
M.B. Benedetti*, V.F. Fontanari, C.S. Santus; University of Pisa, Italy |
18.10 |
Close of Day 2 |
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Wednesday 17 September 2008 |
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Session 9: Probabilistic approaches |
08:30 |
Fatigue variability of a Ni-base superalloy
R.J. Morrissey*, R. John; Air Force Research Laboratory, USA |
09:00 |
Fatigue weakest-link density and strength distribution: Materials fatigue properties
T. Zhai*¹, J.X. Li¹, T. Li¹, X.P. Jiang¹, J.C. Li¹, G.H. Bray², et al; ¹University of Kentucky, USA, ²Alcoa Technical Center, USA |
09:30 |
Study of fatigue variability in Ti-6Al-4V
P.J. Golden*, R. John; Air Force Research Laboratory, USA |
10:00 |
Nondeterministic fatigue crack growth predictive modeling
R.L. Holtz*; US Naval Research Laboratory, USA |
10:30 |
Refreshments |
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Session 10: Systematic materials studies - I |
11:00 |
KEYNOTE
Crack tip deformation fields and fatigue crack growth rates in Ti-6Al-4V
A.M. Korsunsky*¹, D. Dini², et al; ¹University of Oxford, UK, ²Imperial College, UK |
11:40 |
Improved test methods for measuring fatigue crack growth rates in aerospace materials
J.C. Newman*¹, Y. Yamada¹, J.J. Ruschau²; ¹Mississippi State University, USA, ²University of Dayton Research Institute, USA |
12:10 |
Fatigue crack growth of aluminum alloys at ultra high vacuum (10-10 torr)
J.J. Williams¹, N. Chawla¹*, A.K. Vasudevan²; ¹Arizona State University, USA, ²Office of Naval Research,USA |
12:40 |
Effect of load ratio on fatigue lives and crack propagation behavior of the extruded
magnesium alloy
S. Ishihara*¹, A. McEvily², M. Sato¹, K. Taniguchi¹, T. Goshima¹; ¹University of Toyama, Japan,
²University of Connecticut, USA |
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Close of Day 3 and free time |
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Thursday 18 September 2008 |
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Session 11: Systematic materials studies -II |
08:30 |
Experimental and numerical investigation of thickness effects in plasticity-induced fatigue
crack closure
P.F.P. de Matos, D. Nowell*; University of Oxford, UK |
09:00 |
Subsurface fatigue crack generation and strain incompatibility near grain boundaries for a
nitrogen-strengthened austenitic steel at cryogenic temperature
O. Umezawa; Yokohama National University, Japan |
09:30 |
3D crack closure measurement using laboratory x ray tomography and extended image
correlation
J.-Y. Buffiere*¹,², N. Limodin¹, J.-P. Tinnes¹, J. Rethore¹, S. Roux²,¹, F. Hild²,¹; ¹Universite de Lyon
INSA-Lyon, France, ²ENS Cachan, France |
10:00 |
Refreshments |
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Session 12: Systematic materials studies - III |
10:30 |
Transformation of mechanical defects into fatigue cracks - prediction of the effects of
scratches on service life
A. Cini*, P.E. Irving; Cranfield University, UK |
11:00 |
Dislocation microstructure evolution in DSS under uniaxial and biaxial cyclic loadings
P. Evrard*¹, S. Herenu², V. Aubin¹, I. Alvarez-Armas², S. Degallaix¹; ¹Ecole Centrale de Lille, France,
²Instituto de Fisica CONICET, Argentina |
11:30 |
Cyclic effects on a nano-particle-strengthened superalloy – in-situ neutron-diffraction and
small-angle-neutron scattering measurements
E.-W. Huang*¹, P.K. Liaw¹, E. Oliver², Y. Liu³, L. Porcae³, J.-J. Kai4, W.R. Chen5 et al; ¹University of Tennessee, USA, ²Rutherford Appleton Laboratory, UK, ³National Institute for Standards and Technology, USA, 4National Tsing Hua University, South Korea, 5Oak Ridge National Laboratory, USA |
12:00 |
An experimental investigation of fatigue crack growth of stainless steel 304L
S. Kalnaus*¹, F. Fan¹, A.K. Vasudevan², Y. Jiang¹; ¹University of Nevada, Reno, USA, ²Office of Naval Research, USA |
12:30 |
Poster viewing
(Poster session 3 – Comprehensive experimental studies) |
13:10 |
Lunch |
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Session 13: Crack initiation and growth from contacts |
14:00 |
The effect of FOD on the fatigue strength of aluminum
D. Lanning*¹, B. Slade¹, C. Catacora²; ¹Embry-Riddle Aeronautical University, USA, ²Virginia Tech,
USA |
14:30 |
Different approaches to estimate life in fretting fatigue with spherical and cylindrical
contact
C. Navarro*, J. Vázquez, S. Muñoz, J. Domínguez; University of Seville, Spain |
15:00 |
Multiaxial fretting fatigue testing for splined couplings
D. Houghton*, P.M. Wavish, S.B. Leen, E.J. Williams, I.R. McColl; University of Nottingham, UK |
15:30 |
Refreshments |
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Session 14: Analysis and modelling approaches |
16:00 |
Propagation and interaction of multiple cracks in a tensile specimen using FRANC3D crack
growth simulation
K.W. Barlow; Naval Air Systems Command, USA |
16:30 |
Point load weight function solutions for part-through cracks in finite thickness plates
X. Wang*¹, G. Glinka²; ¹Carleton University, Canada, ²University of Waterloo, Canada |
17:00 |
Simple stress intensity factor method for a crack from a cutout using a stiffness modified
shear only finite element calculation
M.R. Urban*; Sikorsky Aircraft, USA |
17:30 |
New fatigue life calculation method for quenched and tempered steel SAE 4140
P. Starke*, F. Walther, D. Eifler; University of Kaiserslautern, Germany |
18:10 |
Close of Day 4 |
19:30 |
Conference banquet |
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Friday 19 September 2008 |
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Session 15: Variable amplitude fatigue - I |
08:30 |
Crack growth prediction for aircraft structural integrity using spectrum fatigue data
W. Zhuang*, M. McDonald, L. Molent; Defence Science and Technology Organisation, Australia |
09:00 |
Enhanced life prediction for airframe structures under variable amplitude fatigue loading
L. Wang, Y. Chen, W. Tiu, Y. Xu*; University of Hertfordshire, UK |
09:30 |
Application of the UniGrow model to fatigue crack growth prediction under spectrum loading
S.M. Mikheevskiy*, G. Glinka; University of Waterloo, Canada |
10:00 |
The effect of loading sequences on fatigue damage under hard landing
J.X. Tao*; Messier-Dowty Ltd, UK |
10:30 |
Refreshments |
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Session 16: Variable amplitude fatigue -II |
11:00 |
Influence of foreign object damage on fatigue crack growth of gas turbine aerofoils
under complex loading conditions
J. Tong*, J. Byrne, R. Hall; University of Portsmouth, UK |
11:30 |
Experimental observation and modeling of the retardation of fatigue crack propagation
under the combination of mixed-mode single overload
J. Lee¹, B. Choi*²; ¹LG Chemicals, South Korea, ²MecKorea University, South Korea |
12:00 |
Fatigue of 7075-t651 aluminum alloy under constant and variable amplitude loadings
E.U. Lee*¹, G. Glinka², A.K. Vasudevan³; ¹Naval Air Warfare Center Aircraft Division, USA,
²University of Waterloo, Canada, ³Office of Navel Research, USA |
12:30 |
Fractographic measurement of crack growth rates for small cracks from simple
sequences in AA7050-T7451
P.D. White*, S.A. Barter; Defence Science and Technology Organisation, Australia |
13:00 |
Closing remarks |
13:10 |
Lunch |
