| Strain-induced precipitation behaviour in hot rolled strip steel EV Pereloma, BR Crawford, PD Hodgson Materials Science and Engineering: A 299 (1-2), 27-37, 2001 | 119 | 2001 |
| The EIFS distribution for anodized and pre‐corroded 7010‐T7651 under constant amplitude loading BR Crawford, C Loader, AR Ward, C Urbani, MR Bache, SH Spence, ... Fatigue & Fracture of Engineering Materials & Structures 28 (9), 795-808, 2005 | 69 | 2005 |
| Can pitting corrosion change the location of fatigue failures in aircraft? BR Crawford, C Loader, Q Liu, TJ Harrison, PK Sharp International journal of fatigue 61, 304-314, 2014 | 38 | 2014 |
| Differing microstructural properties of 7075-T6 sheet and 7075-T651 extruded aluminium alloy TJ Harrison, BR Crawford, M Janardhana, G Clark Procedia Engineering 10, 3117-3121, 2011 | 27 | 2011 |
| Predicting the complete tensile properties of additively manufactured Ti-6Al-4V by integrating three-dimensional microstructure statistics with a crystal plasticity model F Azhari, C Wallbrink, Z Sterjovski, BR Crawford, A Menzel, D Agius, ... International Journal of Plasticity 148, 103127, 2022 | 23 | 2022 |
| Assessment of the effect of pitting corrosion on the safe life prediction of the P3-C. A Shekhter, C Loader, W Hu, BR Crawford | 21 | 2007 |
| The effect of pitting corrosion on the safe-life prediction of the Royal Australian Air Force P-3C Orion aircraft A Shekhter, BR Crawford, C Loader, W Hu Engineering Failure Analysis 55, 193-207, 2015 | 19 | 2015 |
| Modelling the effects of intergranular corrosion around a fastener hole in 7075-T651 aluminium alloy TJ Harrison, BR Crawford, M Brandt, G Clark Computational materials science 84, 74-82, 2014 | 15 | 2014 |
| Equivalent Crack Size Modelling of Corrosion Pitting in an AA7050-T7451 Aluminium Alloy and its Implications for Aircraft Structural Integrity. BR Crawford, PK Sharp | 15 | 2012 |
| A proposed roadmap for transitioning DSTO's corrosion structural integrity research into Australian Defence Force service BR Crawford, C Loader, PK Sharp DSTOTR-2475, Oct, 2010 | 11 | 2010 |
| The role of reinforcement particles during fatigue cracking of a micral-20 [TM]-reinforced 6061 alloy BR Crawford, JR Griffiths Fatigue and Fracture of Engineering Materials and Structures 22, 811-820, 1999 | 10 | 1999 |
| A comparison of statistically equivalent and realistic microstructural representative volume elements for crystal plasticity models F Azhari, W Davids, H Chen, SP Ringer, C Wallbrink, Z Sterjovski, ... Integrating Materials and Manufacturing Innovation 11 (2), 214-229, 2022 | 9 | 2022 |
| DSTO aircraft structural prognostic health monitoring program for corrosion prevention and control R Bartholomeusz, B Crawford, C Davis, S Galea, B Hinton, G McAdam, ... | 8 | 2004 |
| Fatigue in the presence of corrosion pitting in an aerospace aluminium alloy SH Spence, NM Williams, AJ Stonham, MR Bache, AR Ward, WJ Evans, ... Proceedings of the 8th International Fatigue Congress, 2-7, 2002 | 8 | 2002 |
| Predicting the likely causes of early crack initiation for extruded aircraft components containing intergranular corrosion TJ Harrison, BR Crawford, C Loader, G Clark, M Brandt International Journal of Fatigue 82, 700-707, 2016 | 7 | 2016 |
| Structural Integrity Assessment of Corrosion in Aircraft Structures BR Crawford, C Loader, PK Sharp, G Clark, C Urbani, D Hay, A Ward, ... DSTO-RR-0294, Melbourne, DSTO, 2005 | 7 | 2005 |
| Development and demonstration of an holistic structural integrity process using the initial discontinuity state concept for 7050-T7451 aluminum TB Mills, KT Honeycutt, CL Brooks, PK Sharp, C Loader, B Crawford USAF Aircraft Structural Integrity Program Conference, Memphis, TN, USA, 2004 | 7 | 2004 |
| The effect of pitting corrosion on the position of aircraft structural failures BR Crawford, C Loader, PK Sharp | 6 | 2004 |
| A model for predicting the stress concentration of intergranular corrosion around a fastener hole TJ Harrison, BR Crawford, G Clark, M Brandt Advanced Materials Research 891, 242-247, 2014 | 5 | 2014 |
| Effect of Anodising on the Fatigue Properties of Aluminium Alloys. BR Crawford | 4 | 2013 |
peter hodgsondeakin universityVerified email at deakin.edu.au
