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Chris Loader

Observed names: C. LOADER, C. Loader, C.B Loader, C.B. Loader, Christopher Loader, Loader, C.
OpenAlex ID: A5013519005
A smart repair system for polymer matrix composites
2001 · S.M Bleay, C.B Loader, et al. · Composites Part A Applied Science and Manufacturing · 410
Microstructure evolution and fatigue behavior of 2124 aluminum processed by ECAE with back pressure
2006 · R. Lapovok, C. Loader, et al. · Materials Science and Engineering A · 59
The EIFS distribution for anodized and pre‐corroded 7010‐T7651 under constant amplitude loading
2005 · B. R. CRAWFORD, C. LOADER, et al. · Fatigue & Fracture of Engineering Materials & Structures · 49
Can pitting corrosion change the location of fatigue failures in aircraft?
2013 · Bruce R. Crawford, Chris Loader, et al. · International Journal of Fatigue · 29
The effect of pitting corrosion on the safe-life prediction of the Royal Australian Air Force P-3C Orion aircraft
2015 · A. Shekhter, B.R. Crawford, et al. · Engineering Failure Analysis · 17
Effect of High Temperature Exposure on the Mechanical Properties of Cold Expanded Open Holes in 7050-T7451 Aluminium Alloy
2008 · Q. Liu, P S Baburamani, et al. · Defense Technical Information Center (DTIC) · 6
A Demonstration using Low-kt Fatigue Specimens of a Method for Predicting the Fatigue Behaviour of Corroded Aircraft Components
2013 · Bruce R. Crawford, Chris Loader, et al. · 5
Assessment of the Effect of Pitting Corrosion on the Safe Life Prediction of the P-3C
2007 · Alexandra Shekhter, Christopher Loader, et al. · Defense Technical Information Center (DTIC) · 5
The Incorporation of Pitting Corrosion Damage into F-111 Fatigue Life Modelling
2002 · Mills, T., Sharp, P. K., et al. · Defense Technical Information Center (DTIC) · 5
Diamond fibres by a hot filament CVD process
1997 · P.W. Griffith, A. Wisbey, et al. · Diamond and Related Materials · 5
Predicting the likely causes of early crack initiation for extruded aircraft components containing intergranular corrosion
2015 · Timothy J. Harrison, Bruce R. Crawford, et al. · International Journal of Fatigue · 4
The Effect Of Pitting Corrosion On The Position Of Aircraft Structural Failures
2004 · Bruce R. Crawford, Chris Loader, et al. · 4
Review of F-111 Structural Materials
2001 · T. Mills, Graham Clark, et al. · 4
Experimental and Modeling Study of the Effect of Corrosion Pitting on Fatigue Failure Locations in Aircraft Components
2014 · Bruce R. Crawford, Chris Loader, et al. · Advanced materials research · 3
The Development of Retrogression and Re-aging to Manage Environmental Degradation in Australian Defence Force Aircraft
2018 · Bruce R. Crawford, Alexandra Shekhter, et al. · Materials Performance and Characterization · 2
Aircraft Structural Integrity: Corrosion Effects
2019 · Bruce Crawford, Chris Loader, et al. · CRC Press eBooks · 1
Overview of USTO's past and future research into corrosion structural integrity
2011 · BR Crawford, Christopher Loader, et al. · 1
Microstructural implications of chromic acid (type IB) and sulphuric acid (type IC) anodising on the fatigue performance of AA7085-T7452 aluminium alloy
2017 · Suzana Turk, Alexandra Shekhter, et al.
Effect of anodising treatment on equivalent crack size of the 7XXX aluminium alloy
2015 · Alexandra Shekhter, P. K. Sharp, et al.
Retrogression and Re-Ageing In-Service Demonstrator Reliability Trials: Stage 3 Component Test Report
2012 · Chris Loader, Brett Crawford, et al.
Hot isostatic pressing of titanium alloy/SiC fiber metal matrix composites
1996 · C.M. Ward‐Close, Miriam Wood, et al. · OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information)
Works count: 23
Citation count: 609
H-index: 6
I10-index: 5
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