The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue research in Australia and New Zealand for...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue research in Australia and New Zealand for...
Printed in Great Britain Biostatistics Advance Access published March 23, 2006 (2009)
G Clark, Maria De Iorio, Robert C Griffiths
Haplotype data capture the genetic variation among individuals in a population and among populations. An understanding of this variation and the ancestral history of haplotypes is important in...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue research in Australia and New Zealand for...
Russo, S, Sharp, P, Dhamari, R, Mills, T, Hinton, B, Clark, G, ...
Fatigue results of 1 1/2 dog-bone jointed specimens manufactured from 7075-T6 aluminium alloy indicated that the application of corrosion preventative compounds (CPCs) at the faying surfaces slightly...
Frequency-Shaping with Spatial Compensators (2008)
G. Clark Smith, Robert L. Clark, G. Clark, Robert L. Clark
Citations (this article cites 9 articles hosted on the
Prof Anthony, C. Davies, Dr Sergio, A. Velastin, Mr David, A. Fraser, ...
There are at least two contexts in which distributed multi-processor real-time (R-T) systems present increasingly difficult technical challenges to continuing the ‘synchronous-digital-design ’...
Efficacy and Sustainability of a (2008)
Cynthia Scheideman-miller, Mha Pamela, G. Clark, Post Bob, ...
Sustainability and appropriateness of care are important components for healthcare systems as they begin integrating telemedicine/telehealth as an integral part of their healthcare delivery. Part of...
Kings Buildings, Edinburgh EH9 3JZ. (2007)
Recent research has investigated ways in which generally distributed random variables may be incorporated into stochastic process algebra. These proposals allow the arbitrary use of such variables,...
This document has been prepared for presentation to the 30th Conference of the International Committee on Aeronautical Fatigue scheduled to be held in Naples, Italy, 14th and 15th May 2007. Brief...
This document has been prepared for presentation to the 30th Conference of the International Committee on Aeronautical Fatigue scheduled to be held in Naples, Italy, 14th and 15th May 2007. Brief...
This document has been prepared for presentation to the 30th Conference of the International Committee on Aeronautical Fatigue scheduled to be held in Naples, Italy, 14th and 15th May 2007. Brief...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue work in Australia and New Zealand for...
Modelling of stable tearing in aircraft structures (2005)
Liu, Q., Hamel, P., Hu, W., Sharp, P.K., Lahousse, A., Clark, G.
Fatigue crack growth in metallic structures remains one of the main threats to aircraft structural integrity, and is the subject of extensive research worldwide in an attempt to assess existing...
CD molecules 2005: human cell differentiation molecules (2005)
Zola, Heddy, Swart, B., Nicholson, I. C., Aasted, B., Bensussan, A., Boumsell, L., ...
CD molecules 2005: human cell differentiation molecules (2005)
Zola, Heddy, Swart, B., Nicholson, I. C., Aasted, B., Bensussan, A., Boumsell, L., ...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue work in Australia and New Zealand for...
Modelling of stable tearing in aircraft structures (2005)
Liu, Q., Hamel, P., Hu, W., Sharp, P.K., Lahousse, A., Clark, G.
Fatigue crack growth in metallic structures remains one of the main threats to aircraft structural integrity, and is the subject of extensive research worldwide in an attempt to assess existing...
The EIFS distribution for anodised and corroded 7010-T7651 under constant amplitude loading (2005)
Crawford, B.R., Loader, C., Ward, A.R., Urbani, C., Bache, M.R., Spence, S.H., ...
This paper reports results from SICAS, an experimental programme to evaluate the effectiveness of the equivalent initial flaw size (EIFS) approach in managing the structural integrity effects of...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue work in Australia and New Zealand for...
Modelling of stable tearing in aircraft structures (2005)
Liu, Q., Hamel, P., Hu, W., Sharp, P.K., Lahousse, A., Clark, G.
Fatigue crack growth in metallic structures remains one of the main threats to aircraft structural integrity, and is the subject of extensive research worldwide in an attempt to assess existing...
The EIFS distribution for anodised and corroded 7010-T7651 under constant amplitude loading (2005)
Crawford, B.R., Loader, C., Ward, A.R., Urbani, C., Bache, M.R., Spence, S.H., ...
This paper reports results from SICAS, an experimental programme to evaluate the effectiveness of the equivalent initial flaw size (EIFS) approach in managing the structural integrity effects of...
The EIFS distribution for anodised and corroded 7010-T7651 under constant amplitude loading (2005)
Crawford, B.R., Loader, C., Ward, A.R., Urbani, C., Bache, M.R., Spence, S.H., ...
This paper reports results from SICAS, an experimental programme to evaluate the effectiveness of the equivalent initial flaw size (EIFS) approach in managing the structural integrity effects of...
Liu, Q., Ding, K., Ye, L., Rey, C., Barter, S. A., Sharp, P. K., ...
Laser shock peening (LSP) is a promising surface treatment for fatigue life extension of metallic materials. The benefits include deeper residual stresses (>1 mm) and a smoother surface finish than...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue work in Australia and New Zealand for...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue work in Australia and New Zealand for...
The Australasian delegate to the International Committee on Aeronautical Fatigue (ICAF) is responsible for preparing a review of aeronautical fatigue work in Australia and New Zealand for...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
Fatigue life recovery in aluminium alloy aircraft structure (2002)
Sharp, P.K., Liu, Q., Barter, S.A., Baburamani, P., Clark, G.
Abstract This paper presents the results of several DSTO research programmes which investigated the effectiveness of the fatigue life enhancement method used on RAAF F/A-18 aircraft – glass bead...
Initiation and early growth of fatigue cracks in an aerospace aluminium alloy (2002)
Barter, S.A., Sharp, P.K., Holden, G., Clark, G.
Material imperfections usually play a substantial role in the early stages of fatigue cracking. This article presents some observations concerning fatigue crack initiating flaws and early crack...
The use of mycophenolate mofetil suspension in pediatric renal allograft recipients (2001)
Birk, P., Greenbaum, L., Lirenman, D., Tang, H., Walker, R., Klamerus, K., ...
Mycophenolate mofetil (MMF) is widely used to prevent acute rejection in adults after renal, cardiac, and liver transplantation. This study investigated the safety, tolerability, and pharmacokinetics...
The effect of peening on the fatigue life of 7050 aluminium alloy (2001)
Many changes in the design and manufacture of high-performance military aircraft - for example, the use of highly optimised design and the use of higher-strength materials have led to an...
Review of F-111 structural materials (2001)
Mills, T., Clark, G., Loader, C., Sharp, P.K., Schmidt, R.
Safety by inspection has been the key to protecting the F-111 fleet since the early 1970s. The ageing of the F-111 fleet in conjunction with a significant increase in planned retirement date has...
An inventory of Lapita sites containing dentate-stamped pottery (2001)
Anderson, A., Bedford, S., Clark, G., Lilley, I., Sand, C., Summerhayes, G., ...
An inventory of Lapita sites containing dentate-stamped pottery (2001)
Anderson, A., Bedford, S., Clark, G., Lilley, I., Sand, C., Summerhayes, G., ...
HIV gp120 receptors on human dendritic cells (2001)
Turville, S. G., Arthos, J., MacDonald, K., Lynch, G., Naif, H., Clark, G., ...
Dendritic cells (DCs) are important targets for human immunodeficiency virus (HIV) because of their roles during transmission and also maintenance of immune competence. Furthermore, DCs are a key...
The effect of peening on the fatigue life of 7050 aluminium alloy (2001)
Many changes in the design and manufacture of high-performance military aircraft - for example, the use of highly optimised design and the use of higher-strength materials have led to an...
Review of F-111 structural materials (2001)
Mills, T., Clark, G., Loader, C., Sharp, P.K., Schmidt, R.
Safety by inspection has been the key to protecting the F-111 fleet since the early 1970s. The ageing of the F-111 fleet in conjunction with a significant increase in planned retirement date has...
Recent research has investigated ways in which generally distributed random variables may be incorporated into stochastic process algebra (SPA). These proposals allow the arbitrary use of such...
The effect of peening on the fatigue life of 7050 aluminium alloy (2001)
Many changes in the design and manufacture of high-performance military aircraft - for example, the use of highly optimised design and the use of higher-strength materials have led to an...
Review of F-111 structural materials (2001)
Mills, T., Clark, G., Loader, C., Sharp, P.K., Schmidt, R.
Safety by inspection has been the key to protecting the F-111 fleet since the early 1970s. The ageing of the F-111 fleet in conjunction with a significant increase in planned retirement date has...
The PS complex produces the nominal LHC beam (2000)
Benedikt, Michael, Blas, A, Borburgh, J, Cappi, R, Chanel, M, Chohan, V, ...
The LHC [1] will be supplied, via the SPS, with protons from the pre-injector chain comprising Linac2, PS Booster (PSB) and PS. These accelerators have under-gone a major upgrading programme [2]...
Barter, S., Molent, L., Sharp, K., Clark, G.
This paper discusses the application of a novel rework/repair method developed at AMRL for fatigue-critical aircraft parts. The approach is based on estimating the depth of any current cracking, and...
Effects of exfoliation corrosion on the fatigue life of two high-strength aluminium alloys (2000)
Sharp, K., Mills, T., Russo, S., Clark, G., Liu, Q.
A 2D model proposed by some of the authors to describe exfoliation corrosion 2-3 years ago took account of material loss and introduced the concept of a process zone to account for the reduction in...
Recent advances in modelling exfoliation corrosion (2000)
Sharp, K., Mills, T., Clark, G., Russo, S.
Exfoliation corrosion is a common problem with many of the older aluminium alloys used in RAAF transport aircraft. The poor understanding of the effect of exfoliation corrosion on fatigue life has...
Barter, S., Molent, L., Sharp, K., Clark, G.
This paper discusses the application of a novel rework/repair method developed at AMRL for fatigue-critical aircraft parts. The approach is based on estimating the depth of any current cracking, and...
Effects of exfoliation corrosion on the fatigue life of two high-strength aluminium alloys (2000)
Sharp, K., Mills, T., Russo, S., Clark, G., Liu, Q.
A 2D model proposed by some of the authors to describe exfoliation corrosion 2-3 years ago took account of material loss and introduced the concept of a process zone to account for the reduction in...
Recent advances in modelling exfoliation corrosion (2000)
Sharp, K., Mills, T., Clark, G., Russo, S.
Exfoliation corrosion is a common problem with many of the older aluminium alloys used in RAAF transport aircraft. The poor understanding of the effect of exfoliation corrosion on fatigue life has...
Barter, S., Molent, L., Sharp, K., Clark, G.
This paper discusses the application of a novel rework/repair method developed at AMRL for fatigue-critical aircraft parts. The approach is based on estimating the depth of any current cracking, and...
Effects of exfoliation corrosion on the fatigue life of two high-strength aluminium alloys (2000)
Sharp, K., Mills, T., Russo, S., Clark, G., Liu, Q.
A 2D model proposed by some of the authors to describe exfoliation corrosion 2-3 years ago took account of material loss and introduced the concept of a process zone to account for the reduction in...
Recent advances in modelling exfoliation corrosion (2000)
Sharp, K., Mills, T., Clark, G., Russo, S.
Exfoliation corrosion is a common problem with many of the older aluminium alloys used in RAAF transport aircraft. The poor understanding of the effect of exfoliation corrosion on fatigue life has...
Russo, S.G., Sharp, P.K., Dharma, R., Hinton, B.R.W., Shankar, K., Clark, G.
Corrosion and fatigue are major factors in determining the structural integrity and life expectancy of aging aircraft. The presence of corrosion on airframe structures can have a detrimental effect...
Russo, S.G., Sharp, P.K., Dharma, R., Hinton, B.R.W., Shankar, K., Clark, G.
Corrosion and fatigue are major factors in determining the structural integrity and life expectancy of aging aircraft. The presence of corrosion on airframe structures can have a detrimental effect...
Russo, S.G., Sharp, P.K., Dharma, R., Hinton, B.R.W., Shankar, K., Clark, G.
Corrosion and fatigue are major factors in determining the structural integrity and life expectancy of aging aircraft. The presence of corrosion on airframe structures can have a detrimental effect...
Public Institutions and Rural Development (1998)
Clark, G., Bowler, I., Darrall, J., Heaney, D., Ilbery, B.
This paper reports on a multi-national research project conducted in 1994-7 and funded by the EU. The aim was to discover the most effective methods by which public institutions could promote rural...
Izbicka, E., Lawrence, R., Raymond, E., Eckhardt, G., Faircloth, G., Jimeno, J., ...
Background: Ecteinascidin-743 (ET-743), a member of the ecteinascidin family selected for clinical development, is a tetrahydroisoquinolone alkaloid isolated from the marine asci-dian, Ecteinascidia...
The implications of corrosion with respect to aircraft structural integrity (1997)
Cole, G.K., Clark, G., Sharp, P.K.
Increasing economic pressure has encouraged extension of the service lives of many civil and military aircraft fleets beyond their original design goals. Consequently, since the incidence of...
The implications of corrosion with respect to aircraft structural integrity (1997)
Cole, G.K., Clark, G., Sharp, P.K.
Increasing economic pressure has encouraged extension of the service lives of many civil and military aircraft fleets beyond their original design goals. Consequently, since the incidence of...
Retardation and repair of fatigue cracks by adhesive infiltration (1997)
Sharp, P.K., Clayton, J.Q., Clark, G.
This paper presents results which demonstrate that polymeric filler materials, such as low-viscosity epoxies, can be vacuum-infiltrated into fatigue cracks in 7050 aluminium alloy to produce...
The implications of corrosion with respect to aircraft structural integrity (1997)
Cole, G.K., Clark, G., Sharp, P.K.
Increasing economic pressure has encouraged extension of the service lives of many civil and military aircraft fleets beyond their original design goals. Consequently, since the incidence of...
Retardation and repair of fatigue cracks by adhesive infiltration (1997)
Sharp, P.K., Clayton, J.Q., Clark, G.
This paper presents results which demonstrate that polymeric filler materials, such as low-viscosity epoxies, can be vacuum-infiltrated into fatigue cracks in 7050 aluminium alloy to produce...
Retardation and repair of fatigue cracks by adhesive infiltration (1997)
Sharp, P.K., Clayton, J.Q., Clark, G.
This paper presents results which demonstrate that polymeric filler materials, such as low-viscosity epoxies, can be vacuum-infiltrated into fatigue cracks in 7050 aluminium alloy to produce...
Evaluation of innovative NDI methods for detection of widespread fatigue damage (1996)
Sharp, P.K., Rowlands, D.E., Clark, G.
In a fatigue test on a stand-alone F / A-18 FS488 wing carry-through bulkhead, the final failure occurred in a large cross-section, from a fatigue crack size only 6 mm deep. Further evaluation of...
Evaluation of innovative NDI methods for detection of widespread fatigue damage (1996)
Sharp, P.K., Rowlands, D.E., Clark, G.
In a fatigue test on a stand-alone F / A-18 FS488 wing carry-through bulkhead, the final failure occurred in a large cross-section, from a fatigue crack size only 6 mm deep. Further evaluation of...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...
Evaluation of innovative NDI methods for detection of widespread fatigue damage (1996)
Sharp, P.K., Rowlands, D.E., Clark, G.
In a fatigue test on a stand-alone F / A-18 FS488 wing carry-through bulkhead, the final failure occurred in a large cross-section, from a fatigue crack size only 6 mm deep. Further evaluation of...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...
A growth model for catastrophic cracking in an RAAF aircraft (1996)
Goldsmith, N.T., Clark, G., Barter, S.A.
The fatigue failure of a training aircraft wing well before it was expected focussed attention on fatigue crack growth in the lower wing spar. To ensure the safety of the remaining fleet required...
Sharp, P.K., Clayton, J.Q., Clark, G.
Metal and glass-bead peening treatments, widely used throughout the aircraft industry to enhance the fatigue performance of many steels and titanium alloys, are now being routinely applied to...
Sharp, P.K., Clayton, J.Q., Clark, G.
Metal and glass-bead peening treatments, widely used throughout the aircraft industry to enhance the fatigue performance of many steels and titanium alloys, are now being routinely applied to...
Acute haemodynamic and renal effects of cyclosporin and indomethacin in man (1994)
Sturrock, N. D. C., Lang, C. C., Clark, G., Struthers, A. D.
A single oral dose of cyclosporin (12 mg/kg) was given to healthy volunteers (n=9) on day 2 with or without indomethacin pretreatment (100 mg day 1+100 mg day 2). All parameters reported were...
Sharp, P.K., Clayton, J.Q., Clark, G.
Metal and glass-bead peening treatments, widely used throughout the aircraft industry to enhance the fatigue performance of many steels and titanium alloys, are now being routinely applied to...
Management of unanticipated fatigue cracking in RAAF Macchi MB326H aircraft (1993)
Clark, G., Drury, S.C., Jost, G.S.
After the crash of a RAAF Aermacchi MB326H jet trainer in November 1990, a detailed investigation concluded that the cause of the crash was structural failure of the port wing lower main spar as a...
Management of unanticipated fatigue cracking in RAAF Macchi MB326H aircraft (1993)
Clark, G., Drury, S.C., Jost, G.S.
After the crash of a RAAF Aermacchi MB326H jet trainer in November 1990, a detailed investigation concluded that the cause of the crash was structural failure of the port wing lower main spar as a...
Ligand/Receptor Binding for 2,3,7,8-TCDD: Implications for Risk Assessment (1993)
PORTIER, C., TRITSCHER, A., KOHN, M., SEWALL, C., CLARK, G., EDLER, L., ...
There is renewed controversy regarding safe exposure levels for dioxin. At the heart of this controversy is the hypothesis that toxic effects of dioxin are receptor-mediated and therefore a...
Management of unanticipated fatigue cracking in RAAF Macchi MB326H aircraft (1993)
Clark, G., Drury, S.C., Jost, G.S.
After the crash of a RAAF Aermacchi MB326H jet trainer in November 1990, a detailed investigation concluded that the cause of the crash was structural failure of the port wing lower main spar as a...
Measuring the Canopy Net Photosynthesis of Glasshouse Crops (1992)
HAND, D. W., CLARK, G., HANNAH, M.A, THORNLEY, J. H. M., WILSON, J. WARREN
A null balance method is described for measuring net photosynthesis of mature canopies of cucumber and other protected crops over periods of 10 min in a single-span glasshouse (c. 9m × 18m in area)....
Morphology of impact damage growth by fatigue in carbon fibre composite laminates (1991)
This paper outlines initial studies of the mechanisms of damage growth in thick, carbon fibre composite laminates. Damage was introduced in the laminate by low-energy impact representative of a...
Application of ultrasonic C-scanning to aerospace composites (1991)
Organic-matrix fibre-reinforced composites are used widely in civil and military aircraft. They are however particularly sensitive to impact damage, and there is a need for a non-destructive...
Modelling residual stresses and fatigue crack growth at cold-expanded fastener holes (1991)
This paper describes a model developed for predicting residual stresses and crack growth in residual stress fields, and the application of the model to crack growth from cold-worked fastener holes in...
Morphology of impact damage growth by fatigue in carbon fibre composite laminates (1991)
This paper outlines initial studies of the mechanisms of damage growth in thick, carbon fibre composite laminates. Damage was introduced in the laminate by low-energy impact representative of a...
Application of ultrasonic C-scanning to aerospace composites (1991)
Organic-matrix fibre-reinforced composites are used widely in civil and military aircraft. They are however particularly sensitive to impact damage, and there is a need for a non-destructive...
Modelling residual stresses and fatigue crack growth at cold-expanded fastener holes (1991)
This paper describes a model developed for predicting residual stresses and crack growth in residual stress fields, and the application of the model to crack growth from cold-worked fastener holes in...
Morphology of impact damage growth by fatigue in carbon fibre composite laminates (1991)
This paper outlines initial studies of the mechanisms of damage growth in thick, carbon fibre composite laminates. Damage was introduced in the laminate by low-energy impact representative of a...
Application of ultrasonic C-scanning to aerospace composites (1991)
Organic-matrix fibre-reinforced composites are used widely in civil and military aircraft. They are however particularly sensitive to impact damage, and there is a need for a non-destructive...
Modelling residual stresses and fatigue crack growth at cold-expanded fastener holes (1991)
This paper describes a model developed for predicting residual stresses and crack growth in residual stress fields, and the application of the model to crack growth from cold-worked fastener holes in...
Moisture absorption in graphite/epoxy laminates (1990)
Clark, G., Saunders, D.S., Van Blaricum, T.J., Richmond, M.
This work investigates the uptake of moisture by XAS-914C and AS4/3501-6 graphite/epoxy composite laminates under a range of temperature and humidity conditions. From the experiments, the diffusion...
Moisture absorption in graphite/epoxy laminates (1990)
Clark, G., Saunders, D.S., Van Blaricum, T.J., Richmond, M.
This work investigates the uptake of moisture by XAS-914C and AS4/3501-6 graphite/epoxy composite laminates under a range of temperature and humidity conditions. From the experiments, the diffusion...
Moisture absorption in graphite/epoxy laminates (1990)
Clark, G., Saunders, D.S., Van Blaricum, T.J., Richmond, M.
This work investigates the uptake of moisture by XAS-914C and AS4/3501-6 graphite/epoxy composite laminates under a range of temperature and humidity conditions. From the experiments, the diffusion...
Modelling of impact damage in composite laminates (1989)
A previous investigation into the characteristics of impact damage in carbon fibre laminates indicated that delaminations occur preferentially at certain interfaces. A model is proposed which...
Modelling of impact damage in composite laminates (1989)
A previous investigation into the characteristics of impact damage in carbon fibre laminates indicated that delaminations occur preferentially at certain interfaces. A model is proposed which...
Modelling of impact damage in composite laminates (1989)
A previous investigation into the characteristics of impact damage in carbon fibre laminates indicated that delaminations occur preferentially at certain interfaces. A model is proposed which...
ABBOTT, T. R., GOODWIN, B., CLARK, G., REES, G. J.
Oxygen uptake (Vo2) and carbon dioxide output (Vco2) were measured continuously in four children during cardiopulmonary bypass, using the variation in concentration of a tracer gas, argon, as a...
The magnetization process in rare earth iron laves phase compounds (1979)
Clark, G., Tanner, B., Sery, R., Savage, H.
The ferromagnetic domain structures in single crystals of (Tb0.27Dy0.73)Fe2 and TbFe2 have been studied directly using synchroton X-radiation topography (SXRT) and the magneto-optical Kerr effect. In...