CV
Casper Versteylen
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2 records found
1
Master thesis
(2025)
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L.B. van der Wekken, V. Popovich, M.J.M. Hermans, C.L. Walters, Casper Versteylen, W.J.B. Nederstigt
The survivability of armour steel under multi-threat loading is influenced by microstructural damage initiated by fragment perforation. This damage affects the way the material deforms and fractures under subsequent blast-induced loading. This thesis investigates the failure micro-mechanisms in Armox 440T after perforation by 20 mm Fragment Simulating Projectiles (FSPs) at 900 m/s and 1600 m/s, followed by Drop-Weight Impact (DWI) loading that simulates blast-induced blast wave loading. A multiscale approach using high-speed digital image correlation (DIC), fractography using Optical Microscopy (OM) and Scanning Electron Microscopy (SEM), Electron Backscatter Diffraction (EBSD) with Kernel Average Misorientation (KAM) mapping, and microhardness profiling reveals the microstructural response to plastic deformation and failure by the formation of adiabatic shear bands (ASBs) and the ductile crack growth phenomena.
Fragment perforation produces complex networks of deformed (dASB) and transformed (tASB) adiabatic shear bands concentrated at the hole surface. With increasing FSP velocity, (I) plug and hole size increases, (II) local hardness peaks intensify reaching ≈ 650 HV within tASBs, and (III) The number of ASBs, branching and junction frequency increases. Microcracks are commonly found near dense tASB clusters at the hole surface and internally in tASB junctions indicating a reduced dynamic fracture tolerance.
Under DWI, cracks initiate at the hole surface and initially propagate perpendicular to the length of the plate, then change direction to ≈ 45◦ shear accompanied by pronounced necking. All fracture surfaces show ductile microvoid coalescence behaviour. The crack centre fails under tensile tearing, which transition into shear failure towards the edges. OM and SEM reveal that microcracks from perforation form under microvoid coalescence and void sheeting. EBSD/KAM mapping on adiabatic shear bands shows ultrafine equiaxed grains and low dislocation density within tASBs, confirming severe strain localisation and dynamic recrystallisation.
Collectively, the results show that tASB networks constitute preferential crack paths that lower the energy absorption capacity in blast impact loading. These findings offer new insights into ASB-enabled damage evolution and provide critical microstructural constraints for modelling and design of armour systems capable of withstanding multi-threat environments. ...
Fragment perforation produces complex networks of deformed (dASB) and transformed (tASB) adiabatic shear bands concentrated at the hole surface. With increasing FSP velocity, (I) plug and hole size increases, (II) local hardness peaks intensify reaching ≈ 650 HV within tASBs, and (III) The number of ASBs, branching and junction frequency increases. Microcracks are commonly found near dense tASB clusters at the hole surface and internally in tASB junctions indicating a reduced dynamic fracture tolerance.
Under DWI, cracks initiate at the hole surface and initially propagate perpendicular to the length of the plate, then change direction to ≈ 45◦ shear accompanied by pronounced necking. All fracture surfaces show ductile microvoid coalescence behaviour. The crack centre fails under tensile tearing, which transition into shear failure towards the edges. OM and SEM reveal that microcracks from perforation form under microvoid coalescence and void sheeting. EBSD/KAM mapping on adiabatic shear bands shows ultrafine equiaxed grains and low dislocation density within tASBs, confirming severe strain localisation and dynamic recrystallisation.
Collectively, the results show that tASB networks constitute preferential crack paths that lower the energy absorption capacity in blast impact loading. These findings offer new insights into ASB-enabled damage evolution and provide critical microstructural constraints for modelling and design of armour systems capable of withstanding multi-threat environments. ...
The survivability of armour steel under multi-threat loading is influenced by microstructural damage initiated by fragment perforation. This damage affects the way the material deforms and fractures under subsequent blast-induced loading. This thesis investigates the failure micro-mechanisms in Armox 440T after perforation by 20 mm Fragment Simulating Projectiles (FSPs) at 900 m/s and 1600 m/s, followed by Drop-Weight Impact (DWI) loading that simulates blast-induced blast wave loading. A multiscale approach using high-speed digital image correlation (DIC), fractography using Optical Microscopy (OM) and Scanning Electron Microscopy (SEM), Electron Backscatter Diffraction (EBSD) with Kernel Average Misorientation (KAM) mapping, and microhardness profiling reveals the microstructural response to plastic deformation and failure by the formation of adiabatic shear bands (ASBs) and the ductile crack growth phenomena.
Fragment perforation produces complex networks of deformed (dASB) and transformed (tASB) adiabatic shear bands concentrated at the hole surface. With increasing FSP velocity, (I) plug and hole size increases, (II) local hardness peaks intensify reaching ≈ 650 HV within tASBs, and (III) The number of ASBs, branching and junction frequency increases. Microcracks are commonly found near dense tASB clusters at the hole surface and internally in tASB junctions indicating a reduced dynamic fracture tolerance.
Under DWI, cracks initiate at the hole surface and initially propagate perpendicular to the length of the plate, then change direction to ≈ 45◦ shear accompanied by pronounced necking. All fracture surfaces show ductile microvoid coalescence behaviour. The crack centre fails under tensile tearing, which transition into shear failure towards the edges. OM and SEM reveal that microcracks from perforation form under microvoid coalescence and void sheeting. EBSD/KAM mapping on adiabatic shear bands shows ultrafine equiaxed grains and low dislocation density within tASBs, confirming severe strain localisation and dynamic recrystallisation.
Collectively, the results show that tASB networks constitute preferential crack paths that lower the energy absorption capacity in blast impact loading. These findings offer new insights into ASB-enabled damage evolution and provide critical microstructural constraints for modelling and design of armour systems capable of withstanding multi-threat environments.
Fragment perforation produces complex networks of deformed (dASB) and transformed (tASB) adiabatic shear bands concentrated at the hole surface. With increasing FSP velocity, (I) plug and hole size increases, (II) local hardness peaks intensify reaching ≈ 650 HV within tASBs, and (III) The number of ASBs, branching and junction frequency increases. Microcracks are commonly found near dense tASB clusters at the hole surface and internally in tASB junctions indicating a reduced dynamic fracture tolerance.
Under DWI, cracks initiate at the hole surface and initially propagate perpendicular to the length of the plate, then change direction to ≈ 45◦ shear accompanied by pronounced necking. All fracture surfaces show ductile microvoid coalescence behaviour. The crack centre fails under tensile tearing, which transition into shear failure towards the edges. OM and SEM reveal that microcracks from perforation form under microvoid coalescence and void sheeting. EBSD/KAM mapping on adiabatic shear bands shows ultrafine equiaxed grains and low dislocation density within tASBs, confirming severe strain localisation and dynamic recrystallisation.
Collectively, the results show that tASB networks constitute preferential crack paths that lower the energy absorption capacity in blast impact loading. These findings offer new insights into ASB-enabled damage evolution and provide critical microstructural constraints for modelling and design of armour systems capable of withstanding multi-threat environments.
Hydrogen infrastructure will play a critical role in meeting the future demand for decarbonization. Existing pipelines can be potentially repurposed, and new pipelines will be installed to transport hydrogen gas. Pipelines, especially offshore pipelines, are subjected to cyclic loading which can lead to potential fatigue damage and failure. The fatigue resistance of steel deteriorates under prolonged exposure to pressurized hydrogen due to the hydrogen embrittlement effect.
Hydrogen assisted fatigue crack growth rate (HA-FCGR) is investigated in this study. The influences of various test parameters including hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel are reviewed and analyzed. Existing models to predict the HA-FCGR are also assessed.
An updated Tri-Linear model is proposed to predict the HA-FCGR of carbon steel. The key values associated with the two knee points, which define the shape of the HA-FCGR curve, are expressed as functions of the test parameters and the yield strength of the steel. Fatigue test results digitized from existing literature are utilized to optimize the experimental constants required for the Tri-Linear model. The modeled HA-FCGR curves are compared against experimental data to demonstrate the agreement with the test results.
The updated Tri-Linear model directly correlates the hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel to the predicted HA-FCGR. Facilitated by the strong correlations, the number of experiments required to qualify the pipeline steel under the design and operating conditions can be reduced. ...
Hydrogen assisted fatigue crack growth rate (HA-FCGR) is investigated in this study. The influences of various test parameters including hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel are reviewed and analyzed. Existing models to predict the HA-FCGR are also assessed.
An updated Tri-Linear model is proposed to predict the HA-FCGR of carbon steel. The key values associated with the two knee points, which define the shape of the HA-FCGR curve, are expressed as functions of the test parameters and the yield strength of the steel. Fatigue test results digitized from existing literature are utilized to optimize the experimental constants required for the Tri-Linear model. The modeled HA-FCGR curves are compared against experimental data to demonstrate the agreement with the test results.
The updated Tri-Linear model directly correlates the hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel to the predicted HA-FCGR. Facilitated by the strong correlations, the number of experiments required to qualify the pipeline steel under the design and operating conditions can be reduced. ...
Hydrogen infrastructure will play a critical role in meeting the future demand for decarbonization. Existing pipelines can be potentially repurposed, and new pipelines will be installed to transport hydrogen gas. Pipelines, especially offshore pipelines, are subjected to cyclic loading which can lead to potential fatigue damage and failure. The fatigue resistance of steel deteriorates under prolonged exposure to pressurized hydrogen due to the hydrogen embrittlement effect.
Hydrogen assisted fatigue crack growth rate (HA-FCGR) is investigated in this study. The influences of various test parameters including hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel are reviewed and analyzed. Existing models to predict the HA-FCGR are also assessed.
An updated Tri-Linear model is proposed to predict the HA-FCGR of carbon steel. The key values associated with the two knee points, which define the shape of the HA-FCGR curve, are expressed as functions of the test parameters and the yield strength of the steel. Fatigue test results digitized from existing literature are utilized to optimize the experimental constants required for the Tri-Linear model. The modeled HA-FCGR curves are compared against experimental data to demonstrate the agreement with the test results.
The updated Tri-Linear model directly correlates the hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel to the predicted HA-FCGR. Facilitated by the strong correlations, the number of experiments required to qualify the pipeline steel under the design and operating conditions can be reduced.
Hydrogen assisted fatigue crack growth rate (HA-FCGR) is investigated in this study. The influences of various test parameters including hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel are reviewed and analyzed. Existing models to predict the HA-FCGR are also assessed.
An updated Tri-Linear model is proposed to predict the HA-FCGR of carbon steel. The key values associated with the two knee points, which define the shape of the HA-FCGR curve, are expressed as functions of the test parameters and the yield strength of the steel. Fatigue test results digitized from existing literature are utilized to optimize the experimental constants required for the Tri-Linear model. The modeled HA-FCGR curves are compared against experimental data to demonstrate the agreement with the test results.
The updated Tri-Linear model directly correlates the hydrogen gas pressure, cyclic load ratio and frequency, test temperature, and the yield strength of the steel to the predicted HA-FCGR. Facilitated by the strong correlations, the number of experiments required to qualify the pipeline steel under the design and operating conditions can be reduced.