All Stories

  1. Computing the Durability of WAAM 18Ni-250 Maraging Steel Specimens with Surface Breaking Porosity
  2. Further thoughts on EIDS and the durability analysis of WAAM 18Ni 250 steel with rough surfaces
  3. Analysis of the Effect of Machining of the Surfaces of WAAM 18Ni 250 Maraging Steel Specimens on Their Durability
  4. Crack growth in conventionally manufactured pure nickel, titanium and aluminum and the cold spray additively manufactured equivalents
  5. Computing the durability of WAAM 18Ni 250 maraging steel specimens
  6. Assessment of mechanical and fatigue crack growth properties of wire + arc additively manufactured mild steel components
  7. A Numerical Study into the Effect of Machining on the Interaction between Surface Roughness and Surface Breaking Defects on the Durability of WAAM Ti-6Al-4V Parts
  8. Theoretical Assessment of Cracking in Orthotropic Material under Symmetrical Heat Flow/Mechanical Loading
  9. Distinct Advantages of Circumferential Notch Tensile (CNT) Testing in the Determination of a Threshold for Stress Corrosion Cracking (KISCC)
  10. Computing the Fatigue Life of Cold Spray Repairs to Simulated Corrosion Damage
  11. Fatigue crack growth in epoxy polymer nanocomposites
  12. Characterising crack growth in commercially pure titanium
  13. Modelling the Variability and the Anisotropic Behaviour of Crack Growth in SLM Ti-6Al-4V
  14. Fracture Analysis for a Crack in Orthotropic Material Subjected to Combined 2i-Order Symmetrical Thermal Flux and 2j-Order Symmetrical Mechanical Loading
  15. On the role of the interface on the damage tolerance and durability of cold spray repairs to AA7075-T7351 aluminium alloy wing skins
  16. Surface roughness and porosity reduce component strength on repeated loading
  17. Experimental Studies into the Analysis Required for the Durability Assessment of 7075 and 6061 Cold Spray Repairs to Military Aircraft
  18. Computing the Growth of Small Cracks in the Assist Round Robin Helicopter Challenge
  19. Further Studies into Crack Growth in Additively Manufactured Materials
  20. Requirements and Variability Affecting the Durability of Bonded Joints
  21. Review of Requirements for the Durability and Damage Tolerance Certification of Additively Manufactured Aircraft Structural Parts and AM Repairs
  22. Synchrotron radiation microcomputed tomography for assessing internal cracks in cold spray repairs
  23. Additively manufactured Ti-6Al-4V replacement parts for military aircraft
  24. On the analysis of cracking under a combined quadratic thermal flux and a quadratic mechanical loading
  25. Crack Growth in a Range of Additively Manufactured Aerospace Structural Materials
  26. Representing crack growth in additively manufactured Ti-6Al-4V
  27. Delamination fatigue growth in polymer-matrix fibre composites: A methodology for determining the design and lifing allowables
  28. Effect of corrosion and fatigue on the remaining life of structures and its implication to additive manufacturing
  29. Crack Growth From Naturally Occurring Material Discontinuities
  30. Multiplicative Manufacturing and Aircraft Sustainment
  31. Practical Computational Fracture Mechanics for Aircraft Structural Integrity
  32. Applications of SPD to Enhance the Structural Integrity of Corroded Airframes
  33. Delamination Growth in Polymer-Matrix Fibre Composites and the Use of Fracture-Mechanics Data for Material Characterization and Life Prediction
  34. Computing the Growth of Naturally-Occurring Disbonds in Adhesively-Bonded Joints
  35. Crack growth: Does microstructure play a role?
  36. Application of SPD to Enhance the Structural Integrity of Fuseage Skins and Centre Barells
  37. The F111C Wing Pivot Fitting Repair and its Implications for the Design/Assessment of Bonded Joints and Composite Repairs
  38. Repair of Multisite Damage in Civil Transport Aircraft: An Example of the Damage-Tolerant Design of Composite Repairs
  39. Examining the application of the Hartman-Schijve equation to the analysis of cyclic fatigue fracture of polymer-matrix composites
  40. Thermoelastic Analysis for Two Collinear Cracks in an Orthotropic Solid Disturbed by Antisymmetrical Linear Heat Flow
  41. Delamination growth in polymer-matrix fibre composites and the use of fracture mechanics data for material characterisation and life prediction
  42. How is product data managed during product development and in-service?
  43. On the analysis of bonded step lap joints
  44. On the interaction between corrosion and fatigue which determines the remaining life of bridges
  45. Life cycle analysis of steel railway bridges
  46. An engineering approach to the fracture assessment of hopper wagons
  47. On the USAF ‘risk of failure’ approach and its applicability to composite repairs to metal airframes
  48. The USAF characteristic k approach for cracks growing from small material discontinuities under combat aircraft and civil aircraft load spectra
  49. Crack growth at fastener holes containing intergranular cracking
  50. A study into the ability of SPD to restore the buckling strength and modes of rib stiffened panels with simulated stress corrosion cracks
  51. Thoughts on the scatter seen in cyclic Mode I fatigue delamination growth in DCB tests
  52. Crack growth in a naturally corroded bridge steel
  53. Influence of cyclic stress intensity threshold on the scatter seen in cyclic mode i fatigue delamination growth in DCB tests
  54. Composite repairs to bridge steels demystified
  55. Cyclic-fatigue crack growth in composite and adhesively-bonded structures: The FAA slow crack growth approach to certification and the problem of similitude
  56. A simple method for calculating the stress intensity factors for complex 3D cracks at a notch
  57. A stress versus crack growth rate investigation (aka stress – cubed rule)
  58. Computing the growth of naturally-occurring disbonds in adhesively-bonded patches to metallic structures
  59. Crack growth from naturally occurring material discontinuities under constant amplitude and operational loads
  60. From NASGRO to fractals: Representing crack growth in metals
  61. The influence of cyclic stress intensity threshold on fatigue life scatter
  62. A simple method based for computing crack shapes
  63. Discussion of the Stress Ratio Effect on the Fatigue Delamination Growth Characterization in FRP Composite Structures
  64. Modelling and predicting fatigue crack growth in structural adhesive joints
  65. Fractals and the lead crack airframe lifing framework
  66. On the Growth of Fatigue Cracks from Material and Manufacturing Discontinuities Under Variable Amplitude Loading
  67. Crack growth at fastener holes containing intergranular cracking
  68. On the potential of supersonic particle deposition to repair simulated corrosion damage
  69. The analysis of stress intensity factors in two interacting collinear asymmetric cracks in a finite plate
  70. Crack Growth from Naturally Occurring Material Discontinuities in Operational Aircraft
  71. Characteristics of the design surface of damage tolerance parameters and their relation to shape optimisation
  72. Supersonic particle deposition as a means for enhancing the structural integrity of aircraft structures
  73. A convenient way to represent fatigue crack growth in structural adhesives
  74. Mode I, II and Mixed Mode I/II delamination growth in composites
  75. Fatigue crack growth and damage tolerance
  76. Application of supersonic particle deposition to enhance the structural integrity of aircraft structures
  77. A study into the interaction of intergranular cracking and cracking at a fastener hole
  78. Tools and methods for addressing the durability of rolling stock
  79. Calculating crack growth from small discontinuities in 7050-T7451 under combat aircraft spectra
  80. Fatigue crack growth in nano-composites
  81. Implications of the lead crack philosophy and the role of short cracks in combat aircraft
  82. Modelling of the lock-in thermography process through finite element method for estimating the rail squat defects
  83. Lock-in thermographic inspection of squats on rail steel head
  84. NDI of Rail Squats and Estimating Defect Size and Location Using Lock-In Thermography
  85. Finite Element Method Study on the Squats Growth Simulation
  86. An investigation of the influence of rail chill on crack growth in a railway wheel due to braking loads
  87. A study into crack growth in a railway wheel under thermal stop brake loading spectrum
  88. The development of combination mechanical contact and thermal braking loads for railway wheel fatigue analysis
  89. Fatigue crack growth in a diverse range of materials
  90. Characterization of the durability of adhesive bonds
  91. A study of the effect of CPCs on fatigue crack propagation in a representative fuselage lap joint specimen
  92. Application of the Hartman–Schijve equation to represent Mode I and Mode II fatigue delamination growth in composites
  93. The tool for assessing the damage tolerance of railway wheel under service conditions
  94. Experimental studies into short crack growth
  95. Observations on fatigue crack growth in a range of materials
  96. On the use of supersonic particle deposition to restore the structural integrity of damaged aircraft structures
  97. Residual Strength Optimisation of a Vent Hole in an Aircraft Component Using a Heuristic Method
  98. An Imidazopiperidine Series of CCR5 Antagonists for the Treatment of HIV: The Discovery ofN-{(1S)-1-(3-Fluorophenyl)-3-[(3-endo)-3-(5-isobutyryl-2-methyl-4,5,6,7-tetrahydro-1H-imidazo[4,5-c]pyridin-1-yl)-8-azabicyclo[3.2.1]oct-8-yl]propyl}acetamide (PF...
  99. Optimal topology design of industrial structures using an evolutionary algorithm
  100. Topology optimisation of a bulkhead component used in aircrafts using an evolutionary algorithm
  101. Application of infrared thermography to study crack growth and fatigue life extension procedures
  102. Lock-in infrared thermography for the evaluation of the structural performance of corrugated paperboard structures
  103. Structures research at the DSTO Centre of Expertise in Structural Mechanics
  104. Cracking in D6ac steel
  105. Fatigue life enhancement of structures using shape optimisation
  106. Damage tolerance analysis of a helicopter component
  107. Structural optimisation of 3D damage tolerant components comparing the biological and genetic algorithm solutions
  108. Designing cutouts for optimum residual strength in plane structural elements
  109. Fatigue crack growth discrepancies with stress ratio
  110. Development of a 3D Biological method for fatigue life based optimisation and its application to structural shape design
  111. Three-dimensional structural design optimisation based on fatigue implementing a genetic algorithm and a non-similitude crack growth law
  112. Three-dimensional fatigue-based structural design optimisation of fuel flow vent holes
  113. Tools for Assessing the Damage Tolerance of Primary Structural Components
  114. A scientific evaluation of the approximate 2D theories for composite repairs to cracked metallic components
  115. The generalised Frost–Dugdale approach to modelling fatigue crack growth
  116. Similitude and the Paris crack growth law
  117. An equivalent block method for computing fatigue crack growth
  118. An approach based on biological algorithm for three-dimensional shape optimisation with fracture strength constrains
  119. Fatigue based three-dimensional structural design optimisation studies implementing the generalised Frost–Dugdale crack growth law
  120. Damage tolerance based design optimisation of a fuel flow vent hole in an aircraft structure
  121. A CAD-based on biological method for designing optimal fatigue life
  122. A fibre optic corrosion fuse sensor using stressed metal-coated optical fibres
  123. Understanding crack growth in fuselage lap joints
  124. Three-dimensional structure optimal design for extending fatigue life by using biological algorithm
  125. Evaluation of spectrum fatigue crack growth using variable amplitude data
  126. Determination of Material Constants for Crack Size-Dependence Crack Growth Model
  127. Determination of Material Constants for Crack Size-Dependence Crack Growth Model
  128. Similitude: Fatigue cracking in steels
  129. Crack growth of physically small cracks
  130. Rail wheel removal and its implication on track life: A fracture mechanics approach
  131. Localized strain measurements using an integration method to process intensity reflection spectra from a chirped FBG
  132. Intragrating strain sensing using a chirped FBG and an integration method
  133. The effect of size on the quantitative estimation of defect depth in steel structures using lock-in thermography
  134. Damage tolerance based shape design of a stringer cutout using evolutionary structural optimisation
  135. Recent developments in fatigue crack growth assessment
  136. An experimental evaluation of crack face energy dissipation
  137. Crack patching revisited
  138. Low-velocity impacts on preloaded GFRP specimens with various impactor shapes
  139. Directional dependence of spectra of fiber Bragg gratings due to excess loss
  140. Predicting the fatigue life and crack aspect ratio evolution in complex structures
  141. NDTE using pulse thermography: Numerical modeling of composite subsurface defects
  142. Interaction of ultrasonic waves with structural damage: A diffraction analogy
  143. Strain-independent temperature measurements using a standard and a Chirped fibre Bragg Grating
  144. Implementation of integration of differences method for extraction of temperature profiles along chirped fibre Bragg gratings
  145. Determination of the position of a localized heat source within a chirped fibre Bragg grating using a Fourier transform technique
  146. Crack patching: Predicting fatigue crack growth
  147. Optimisation of damage tolerant structures using a 3D biological algorithm
  148. Integration Method of Analysis for Intra-grating Sensing with a Chirped Fiber Bragg Grating
  149. Stress intensity factor solutions for finite body with quarter-elliptical flaws emanating from a notch
  150. Assessment of partly circumferential cracks in pipes
  151. Structural optimisation with damage tolerance constraints
  152. An experimental evaluation of fatigue crack growth
  153. Crack patching: an experimental evaluation of fatigue crack growth
  154. An assessment of stress intensity factors for surface flaws in a tubular member
  155. Thermography as a tool for damage assessment
  156. The effect of impactor shape on the impact response of composite laminates
  157. Design of structures for optimal static strength using ESO
  158. Development of life extension strategies for Australian military aircraft, using structural health monitoring of composite repairs and joints
  159. Application of constitutive modelling and advanced repair technology to F111C aircraft
  160. The response of composite structures with pre-stress subject to low velocity impact damage
  161. Stiffness properties for Nucleus standard straight and contour electrode arrays
  162. Modelling creep behaviour of orthotropic composites by the coincident element method
  163. Crack growth at low ?K’s and the Frost‐Dugdale law
  164. Health monitoring of draglines using ultrasonic waves
  165. Weight functions, CTOD, and related solutions for cracks at notches
  166. Weight functions for composite repairs to stiffened panels
  167. Optimization Using Nimrod/O and Its Application to Robust Mechanical Design
  168. Piezomagnetic and piezoelectric poling effects on mode I and II crack initiation behavior of magnetoelectroelastic materials
  169. Crack size and speed interaction characteristics at micro-, meso- and macro-scale
  170. Evaluation of trajectories and contact pressures for the straight nucleus cochlear implant electrode array — a two-dimensional application of finite element analysis
  171. A simple method for computing the stress intensity factors for cracks at notches
  172. Finite element modeling to determine thermal residual strain distribution of bonded composite repairs for structural health monitoring design
  173. In situ health monitoring of bonded composite repairs using a novel fiber Bragg grating sensing arrangement
  174. Assessment of multiple flat elliptical cracks with interactions
  175. Health monitoring of composite repairs and joints using optical fibres
  176. Structural optimisation with fracture strength constraints
  177. Bonded repairs to rib stiffened wing skins
  178. Eleventh International Conference on Composite Structures (ICCS/11), Monash University, Melbourne, Australia, November 2001
  179. Composite repairs to cracked holes under bi-axial loading
  180. Using hybrid element method to solve 3D elliptic crack problems with multi-materials structure
  181. CALCULATION OF THE STRESS INTENSITY FACTOR FOR SMALL-TO-MEDIUM CRACKS WITH APPLICATIONS TO SHAPE OPTIMIZATION PROBLEMS
  182. Adhesively bonded joints under cyclic loading spectra
  183. Repair of Multi-Site Damage
  184. A hybrid formulation for 3D fracture analysis
  185. Numerical Analysis and Design
  186. Compliance measurements for assessing structural integrity
  187. Structural Optimisation With Damage Tolerance Constraints
  188. An implicit algorithm using explicit correctors for the kinematic hardening model with multiple back stresses
  189. Preface
  190. Optical fibre sensors for health monitoring of bonded repair systems
  191. On the analysis of composite structures with material and geometric non-linearities
  192. On the Glinka and Neuber methods for calculating notch tip strains under cyclic load spectra
  193. Shape optimization of damage tolerant structures for static strength and fatigue life
  194. A methodology for structural optimisation with damage tolerance constraints
  195. Composite repairs to rib stiffened panels
  196. On the mechanical behaviour of aging and recycled paper structures under cyclic humidity
  197. Study of multi-site damage of fuselage lap joints
  198. Further studies into interacting 3D cracks
  199. Repairs using fibre reinforced plastics
  200. Repairs using fibre reinforced plastics
  201. Studies in the matrix dominated failures of composite joints
  202. A unified constitutive theory for paper
  203. Assessing and maintaining continued airworthiness in the presence of wide spread fatigue damage: an Australian perspective
  204. Australian developments in the analysis of composite structures with material and geometric nonlinearities
  205. Multiple-site and widespread fatigue damage in aging aircraft
  206. Composite wraps for aging infra-structure
  207. Monitoring of crack growth beneath a bonded repair using Bragg gratings
  208. Load History Effects on Composites Laminates and Composite Repairs
  209. Structural integrity monitoring
  210. Determination of the stress components of an array of piezoelectric sensors: a numerical study
  211. Elastic-plastic finite element analysis of spall formation in gears
  212. An experimental description of the response of paper
  213. Sensor technology for structural integrity monitoring
  214. Determination of arbitrary, non-shearing end-loadings from the bulk stress on the lateral surface of a rectangular prism
  215. Developments in the analysis of interacting cracks
  216. Unified constitutive model for thermoset adhesive, FM73
  217. Airworthiness of composite repairs: Failure mechanisms
  218. Numerical analysis of subsurface crack failure beneath the pitch line of a gear tooth during engagement
  219. A numerical study of MSD in aluminium alloys
  220. A preliminary study into the matrix dominated non-linear behaviour of graphite/epoxy laminates
  221. Continued airworthiness of composite repairs to primary structures for military aircraft
  222. Effects of temperature on the shear stress-strain behaviour of structural adhesives (FM73)
  223. Potential failure mechanisms of bonded composite repairs for metal and concrete
  224. The Use of Piezoelectric Thin Film Sensors for Structural Integrity Monitoring
  225. Bonded-composite repair of representative multi-site damage in a full-scale fatigue-test article
  226. Bonded composite repair of cracked load-bearing holes
  227. Crack growth and repair of multi-site damage of fuselage lap jointsMolent, L. and Jones, R. Eng. Fract. Mech. (Mar. 1993) 44 (4), 627–637
  228. Response of AL 7050—T7451 to complex load spectra
  229. Designing for damage-tolerant composite repairs
  230. A numerical study of crack monitoring in patched structures using a piezoelectric sensor
  231. Residual strength of composites with multiple impact damage
  232. Determination of anti-symmetric end-loadings from volumetric stress on lateral surface of a rectangular bar
  233. Environmental evaluation of repairs to fuselage lap jointsMolent, L. Bridgford, N., Rees, D., and Jones, R. Composite Struct. (1992) 21 (2), 121–130
  234. Crack growth and repair of multi-site damage of fuselage lap joints
  235. Designing for damage tolerant bonded joints
  236. A numerical study of adhesively bonded lap joints
  237. A numerical study of crack monitoring in patched structures using a piezoelectric sensor
  238. Constitutive modelling of the elastic–plastic behaviour of 7050-T7451 aluminium alloy
  239. Environmental evaluation of repairs to fuselage lap joints
  240. Thoughts on energy density, fracture and thermal emission
  241. Determination of Stress Components From Thermoelastic Data Without Boundary Conditions
  242. Repair of impact damaged composites
  243. Determination of symmetric end-loadings from the bulk stress on the lateral surface of a rectangular prism
  244. Bonded Repair of Multi-Site Damage
  245. Analysis of cold-expansion for cracked and uncracked fastener holes
  246. Effects of plasticity on several fracture parameters for impact damage and related problems
  247. A penalty finite element formulation for the analysis of composite structures
  248. Thermomechanical assessment of damage in composites
  249. Understanding delamination behaviour in a circular laminate
  250. A new approach to structural optimization
  251. On the determination of stress components in 3-d from thermoelastic data
  252. Increasing the fatigue life of cracked fastener holes using bonded repairs
  253. Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects
  254. The role of energy related parameters in life enhancement procedures
  255. Thermomechanical analysis of composite specimens
  256. Thermoelastic assessment of damage growth in composites
  257. Numerical analysis of bonded repairs for fastener holes with three-dimensional cracks
  258. An experimental investigation into the effect of impact damage on the compressive strength of step lap joints
  259. Thermomechanical behaviour of composites
  260. A finite element analysis of delamination behaviour in a circular laminate
  261. Assessment of the effect of impact damage in composites: Some problems and answers
  262. Bonded repair of metallic components: Thick sections
  263. Bonded Repair of Aircraft Structures
  264. Assessment of the effect of impact damage in composites: Some problems and answers
  265. Closure effects in delaminated graphite epoxy laminate under compression
  266. Characterisation of pure and mixed mode fracture in composite laminates
  267. Thermoelastic constant or thermoelastic parameter?
  268. A numerical study of two integral type elasto-plastic fracture parameters under cyclic loading
  269. Is fatigue testing of impact damaged laminates necessary?
  270. Computational methods in modern repair technology
  271. Application of the and S criteria in finite element analysis of impact damage at fastener holes in graphite/epoxy laminates under compression
  272. Designing for tolerance to impact damage at fastener holes in graphite/epoxy laminates under compression
  273. Analysis of bonded inserts for the repair of fastener holes
  274. Effect of debonding on adhesively bonded composite to metal joints in compression
  275. An analysis of delamination behaviour
  276. Reducing the effects of rivet holes on fatigue life by adhesive bonding
  277. Compressive Strength of Impact Damaged Graphite Epoxy Laminates
  278. Damage tolerance of graphite/epoxy composites
  279. A Hybrid Contour Method∗
  280. Fracture mechanics technology applied to material evaluation and structure designEdited by: G.C. Sih, N.E. Ryan and R. Jones Martinus Nijhoff Publishers BV (1983) xx + 671 pp Dfl 215 $80.00
  281. Compression failures of damaged graphite epoxy laminates
  282. Repair of mirage III aircraft using the BFRP crack-patching technique
  283. Bonded repairs to surface flaws
  284. Analysis of multi-layer laminates using three-dimensional super-elements
  285. Residual strength of impact-damaged composites
  286. Residual strength of impact damaged composites
  287. BONDED REPAIRS TO SURFACE FLAWS
  288. On the three dimensional analysis of thick laminated plates
  289. Analysis of bonded repairs to damaged fibre composite structures
  290. Fracture Mechanics in Australia
  291. Damage Tolerance of Fibre Composite Laminates
  292. Neutral axis offset effects due to crack patching
  293. Composite Reinforcement of Cracked Aircraft Components
  294. Crack Patching: Analysis and Design
  295. Analysis of composite laminates and fibre composite repair schemes
  296. New thoughts on stropping cracks which emanate from holes
  297. A design study in crack patching
  298. A Note on the Behavior of Plates on an Elastic Foundation
  299. Vibration and buckling of plates at elevated temperatures
  300. A crack opening displacement approach to crack patching
  301. APPLICATION OF BFRP CRACK PATCHING TO MIRAGE III AIRCRAFT
  302. Thermal Considerations in the Patching of Metal Sheets with Composite Overlays
  303. Finite Element Analysis of Patched Cracks
  304. A consistent approach to the fracture of pavements
  305. The Dynamic Analysis of Shallow Spherical Shells
  306. An iterative finite element method using the Kantorovich technique
  307. A simplified approach to the large amplitude vibration of plates and membranes
  308. On the use of special crack tip elements in cracked elastic sheets
  309. Behavior of floating ice sheets
  310. The Vlasov foundation model
  311. Application of the extended Kantorovich method to the vibration of clamped rectangular plates
  312. On the Vlasov and Kerr foundation models
  313. Further studies in the application of the method of constant deflection lines to plate bending problems
  314. An approximate expression for the fundamental frequency of vibration of elastic plates
  315. Transverse vibrations of shallow shells by the method of constant‐deflection contours
  316. A Method of Static Analysis of Shallow Shells
  317. A Simplified Approach to the Analysis of Large Deflections of Plates
  318. Some Practical Implications of Exponential Crack Growth
  319. A multi-scale approach to crack growth
  320. A multi-scale approach to crack growth
  321. Recent Developments in Fatigue Crack Growth
  322. Smart Structures Application to Airworthiness and Repair
  323. An Equivalent Block Approach to Crack Growth