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<title>SAM</title>
<link>https://sam.ensam.eu:443</link>
<description>The DSpace digital repository system captures, stores, indexes, preserves, and distributes digital research material.</description>
<pubDate xmlns="http://apache.org/cocoon/i18n/2.1">Fri, 17 Apr 2026 12:32:40 GMT</pubDate>
<dc:date>2026-04-17T12:32:40Z</dc:date>
<item>
<title>A numerical study of the influence of polydispersity on the behaviour until break of a reinforced hyperelastic material with a cohesive interface</title>
<link>http://hdl.handle.net/10985/9629</link>
<description>A numerical study of the influence of polydispersity on the behaviour until break of a reinforced hyperelastic material with a cohesive interface
TOULEMONDE, Paul-Aymé; DIANI, Julie; GILORMINI, Pierre; DESGARDIN, Nancy
Solid propellants manufacturers commonly monitor the granulometries of the explosive fllers they introduce in the material to pack high fller volume fraction and thus obtain satisfactory energetic performance. However, to our knowledge, the effect of a mix of small and large particles in the micrometric size range in flled elastomers has not yet been fully understood. This work aims at producing a better understanding of the underlying mechanisms that take place in a bidisperse flled elastomer composite under uniaxial loading by using finite element simulations. An original process for creating bidisperse microstructures is proposed and analyzed. The key role of the fller/matrix interface is emphasized through the use of a cohesive zone model. Plane- strain simulations in uniaxial tension of such cells with different fractions of large and small particles are performed.
</description>
<pubDate>Thu, 01 Jan 2015 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/9629</guid>
<dc:date>2015-01-01T00:00:00Z</dc:date>
<dc:creator>TOULEMONDE, Paul-Aymé</dc:creator>
<dc:creator>DIANI, Julie</dc:creator>
<dc:creator>GILORMINI, Pierre</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:description>Solid propellants manufacturers commonly monitor the granulometries of the explosive fllers they introduce in the material to pack high fller volume fraction and thus obtain satisfactory energetic performance. However, to our knowledge, the effect of a mix of small and large particles in the micrometric size range in flled elastomers has not yet been fully understood. This work aims at producing a better understanding of the underlying mechanisms that take place in a bidisperse flled elastomer composite under uniaxial loading by using finite element simulations. An original process for creating bidisperse microstructures is proposed and analyzed. The key role of the fller/matrix interface is emphasized through the use of a cohesive zone model. Plane- strain simulations in uniaxial tension of such cells with different fractions of large and small particles are performed.</dc:description>
</item>
<item>
<title>Platicizer effect on network structure and hydrolytic degradation</title>
<link>http://hdl.handle.net/10985/9634</link>
<description>Platicizer effect on network structure and hydrolytic degradation
DERUE, Isabelle; GILORMINI, Pierre; VERDU, Jacques; VAULOT, Cyril; COQUILLAT, Marie; DESGARDIN, Nancy; VANDENBROUKE, Aude; RICHAUD, Emmanuel
The hydrolytic degradation of fully cured polyester-urethane networks polymerized in the presence of several weight ratios of triacetin was monitored by the residual concentration in elastically active chains obtained from modulus and equilibrium solvent swelling measurements. The presence of triacetin does not change the water uptake but induces a lower rate of degradation. Comparisons were performed with networks in which triacetin was removed before ageing, and with networks in which polyester-urethane was first polymerized and then impregnated by triacetin. Data suggest that the presence of triacetin during polymerization induces the presence of elastically inactive chains such as dangling chains, loops… the hydrolysis of which does not change the elastic properties of the network. This explanation was checked from relaxation measurements by n.m.r and d.m.a, and by the analysis of the soluble fraction generated by hydrolysis.
</description>
<pubDate>Thu, 01 Jan 2015 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/9634</guid>
<dc:date>2015-01-01T00:00:00Z</dc:date>
<dc:creator>DERUE, Isabelle</dc:creator>
<dc:creator>GILORMINI, Pierre</dc:creator>
<dc:creator>VERDU, Jacques</dc:creator>
<dc:creator>VAULOT, Cyril</dc:creator>
<dc:creator>COQUILLAT, Marie</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:creator>VANDENBROUKE, Aude</dc:creator>
<dc:creator>RICHAUD, Emmanuel</dc:creator>
<dc:description>The hydrolytic degradation of fully cured polyester-urethane networks polymerized in the presence of several weight ratios of triacetin was monitored by the residual concentration in elastically active chains obtained from modulus and equilibrium solvent swelling measurements. The presence of triacetin does not change the water uptake but induces a lower rate of degradation. Comparisons were performed with networks in which triacetin was removed before ageing, and with networks in which polyester-urethane was first polymerized and then impregnated by triacetin. Data suggest that the presence of triacetin during polymerization induces the presence of elastically inactive chains such as dangling chains, loops… the hydrolysis of which does not change the elastic properties of the network. This explanation was checked from relaxation measurements by n.m.r and d.m.a, and by the analysis of the soluble fraction generated by hydrolysis.</dc:description>
</item>
<item>
<title>Propellant cohesive fracture during the peel test of a propellant/liner structure</title>
<link>http://hdl.handle.net/10985/13837</link>
<description>Propellant cohesive fracture during the peel test of a propellant/liner structure
TOULEMONDE, Paul-Aymé; GILORMINI, Pierre; JULIE, Diani; DESGARDIN, Nancy; NEVIÈRE, Robert
The integrity of propellant/liner structures in rocket motors is critical to ensure controlled combustion of the engine. In an effort to improve the bonding between the liner and the propellant, it is necessary to characterize it well. Therefore, a propellant–liner structure, bounded thanks to co-curing, has been submitted to a peel test while recording the macroscopic fracture energy and the local displacement field on the propellant-free surface. The experimental setup includes two cameras in order to record the displacement field on the propellant-free surface. Upon loading, the peel force stabilizes quickly due to a cohesive fracture in the propellant, providing access to the fracture energy. While the crack propagates through the propellant, it is observed that only a small localized area is submitted to strain, and most of the structure remains unstrained.
</description>
<pubDate>Mon, 01 Jan 2018 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/13837</guid>
<dc:date>2018-01-01T00:00:00Z</dc:date>
<dc:creator>TOULEMONDE, Paul-Aymé</dc:creator>
<dc:creator>GILORMINI, Pierre</dc:creator>
<dc:creator>JULIE, Diani</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:creator>NEVIÈRE, Robert</dc:creator>
<dc:description>The integrity of propellant/liner structures in rocket motors is critical to ensure controlled combustion of the engine. In an effort to improve the bonding between the liner and the propellant, it is necessary to characterize it well. Therefore, a propellant–liner structure, bounded thanks to co-curing, has been submitted to a peel test while recording the macroscopic fracture energy and the local displacement field on the propellant-free surface. The experimental setup includes two cameras in order to record the displacement field on the propellant-free surface. Upon loading, the peel force stabilizes quickly due to a cohesive fracture in the propellant, providing access to the fracture energy. While the crack propagates through the propellant, it is observed that only a small localized area is submitted to strain, and most of the structure remains unstrained.</dc:description>
</item>
<item>
<title>Thermal oxidation of aromatic epoxy-diamine networks</title>
<link>http://hdl.handle.net/10985/15441</link>
<description>Thermal oxidation of aromatic epoxy-diamine networks
DELOZANNE, Justine; DESGARDIN, Nancy; CUVILLIER, Nicolas; RICHAUD, Emmanuel
The thermal oxidation of DGEBA-DDS (bisphenol A diglycidyl ether + 4,4′-diaminodiphenyl sulfone) and TGMDA-DDS (4,4′-methylenebis(N,N-diglycidylaniline) + 4,4′-diaminodiphenyl sulfone) was performed at 80, 120, and 200 °C and was monitored by FTIR. Oxidation was shown to generate amides and carbonyls. Comparisons were done with model systems displaying some common reactive groups, which highlighted the predominating role of methylene in α position of ether in DGEBA-DDS and methylene in α position of nitrogen hold by TGMDA in TGMDA-DDS. The participation of CH2 in α position of DDS hardener group seems to depend on the temperature and decrease when lowering it. The oxidation of such complex systems must hence be described by a co-oxidation model where each kind of reactive sites is described by its own set of kinetic constants.
</description>
<pubDate>Tue, 01 Jan 2019 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/15441</guid>
<dc:date>2019-01-01T00:00:00Z</dc:date>
<dc:creator>DELOZANNE, Justine</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:creator>CUVILLIER, Nicolas</dc:creator>
<dc:creator>RICHAUD, Emmanuel</dc:creator>
<dc:description>The thermal oxidation of DGEBA-DDS (bisphenol A diglycidyl ether + 4,4′-diaminodiphenyl sulfone) and TGMDA-DDS (4,4′-methylenebis(N,N-diglycidylaniline) + 4,4′-diaminodiphenyl sulfone) was performed at 80, 120, and 200 °C and was monitored by FTIR. Oxidation was shown to generate amides and carbonyls. Comparisons were done with model systems displaying some common reactive groups, which highlighted the predominating role of methylene in α position of ether in DGEBA-DDS and methylene in α position of nitrogen hold by TGMDA in TGMDA-DDS. The participation of CH2 in α position of DDS hardener group seems to depend on the temperature and decrease when lowering it. The oxidation of such complex systems must hence be described by a co-oxidation model where each kind of reactive sites is described by its own set of kinetic constants.</dc:description>
</item>
<item>
<title>Effects of small particles on the mechanical behavior and on the local damage of highly filled elastomers</title>
<link>http://hdl.handle.net/10985/11341</link>
<description>Effects of small particles on the mechanical behavior and on the local damage of highly filled elastomers
TOULEMONDE, Paul-Aymé; DIANI, Julie; GILORMINI, Pierre; DESGARDIN, Nancy; NEVIÈRE, Robert
The mechanical behavior and damage of highly filled elastomers such as propellants is studied experimentally. A model material made of a polyacrylate matrix filled with glass beads and energetic binders filled with ammonium perchlorate and HMX have been formulated. The focus is on materials containing micrometric size particles. The size of fillers was varied from a few microns to hundreds of microns in order to study the impact of the size of particles. The materials stress-strain responses and the volume changes during uniaxial tensile tests have been recorded. Microtomographic slices of strained samples have been obtained in order to look at the type of damage sustained by the acrylate/glass bead materials. It appears that in the presence of large particles, composites showing early prominent crack benefits from the addition of small particles, whereas composites showing well dispersed matrix/particle decohesion without large cracks show no change of behavior when small particles are added.
</description>
<pubDate>Sun, 01 Jan 2017 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/11341</guid>
<dc:date>2017-01-01T00:00:00Z</dc:date>
<dc:creator>TOULEMONDE, Paul-Aymé</dc:creator>
<dc:creator>DIANI, Julie</dc:creator>
<dc:creator>GILORMINI, Pierre</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:creator>NEVIÈRE, Robert</dc:creator>
<dc:description>The mechanical behavior and damage of highly filled elastomers such as propellants is studied experimentally. A model material made of a polyacrylate matrix filled with glass beads and energetic binders filled with ammonium perchlorate and HMX have been formulated. The focus is on materials containing micrometric size particles. The size of fillers was varied from a few microns to hundreds of microns in order to study the impact of the size of particles. The materials stress-strain responses and the volume changes during uniaxial tensile tests have been recorded. Microtomographic slices of strained samples have been obtained in order to look at the type of damage sustained by the acrylate/glass bead materials. It appears that in the presence of large particles, composites showing early prominent crack benefits from the addition of small particles, whereas composites showing well dispersed matrix/particle decohesion without large cracks show no change of behavior when small particles are added.</dc:description>
</item>
<item>
<title>Thermal ageing of bonded assemblies. Effect of adhesive curing degree</title>
<link>http://hdl.handle.net/10985/24723</link>
<description>Thermal ageing of bonded assemblies. Effect of adhesive curing degree
DELOZANNE, Justine; MONTANA, Juan Sebastian; GUINAULT, Alain; DESGARDIN, Nancy; CUVILLIER, Nicolas; RICHAUD, Emmanuel
This paper reports the failure of bonded assemblies submitted to thermal ageing. Adhesives are either fully or incompletely cured. Despite comparable initial properties, depletion of mechanical properties (evaluated from single las shear tests) is faster in the case of incompletely cured polymer. A series of comprehensive experiments were conducted on thin films of adhesive itself and some model systems based on its main components. According to tensile tests and kinetic curves of stable oxidation products detected by Infrared spectroscopy, fully cured epoxy would oxidize faster (because of greater concentration in oxidizable sites). Oxygen diffusivity was observed to be comparable in both systems. It results in a lower thickness of degraded layer in the case of fully cured samples, which explain the results obtained in bonded assemblies.
</description>
<pubDate>Fri, 01 Apr 2022 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/24723</guid>
<dc:date>2022-04-01T00:00:00Z</dc:date>
<dc:creator>DELOZANNE, Justine</dc:creator>
<dc:creator>MONTANA, Juan Sebastian</dc:creator>
<dc:creator>GUINAULT, Alain</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:creator>CUVILLIER, Nicolas</dc:creator>
<dc:creator>RICHAUD, Emmanuel</dc:creator>
<dc:description>This paper reports the failure of bonded assemblies submitted to thermal ageing. Adhesives are either fully or incompletely cured. Despite comparable initial properties, depletion of mechanical properties (evaluated from single las shear tests) is faster in the case of incompletely cured polymer. A series of comprehensive experiments were conducted on thin films of adhesive itself and some model systems based on its main components. According to tensile tests and kinetic curves of stable oxidation products detected by Infrared spectroscopy, fully cured epoxy would oxidize faster (because of greater concentration in oxidizable sites). Oxygen diffusivity was observed to be comparable in both systems. It results in a lower thickness of degraded layer in the case of fully cured samples, which explain the results obtained in bonded assemblies.</dc:description>
</item>
<item>
<title>On the account of a cohesive interface for modeling the behavior until break of highly filled elastomers</title>
<link>http://hdl.handle.net/10985/10434</link>
<description>On the account of a cohesive interface for modeling the behavior until break of highly filled elastomers
TOULEMONDE, Paul-Aymé; DIANI, Julie; GILORMINI, Pierre; DESGARDIN, Nancy
The nonlinear behavior and failure of highly filled elastomers are significantly impacted by the volume fraction, the size and nature of fillers and the matrix stiffness. Original experimental data obtained on glass beads reinforced acrylates and on propellants allow illustrating and discussing the main effects generally observed.  In order to better understand the effects of the microstructure and constitutive parameters on the behavior and failure of highly filled elastomers,  a composite model, represented by a 2D periodic cell with randomly dispersed particles, with an account of a cohesive zone at the filler/matrix interface is used. Finite element simulations with finite strain provide insight on the stress-strain responses dependence to the model parameters and allow defining a failure criterion perceived by the appearance of a critical fibrillar microstructure.
</description>
<pubDate>Fri, 01 Jan 2016 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/10434</guid>
<dc:date>2016-01-01T00:00:00Z</dc:date>
<dc:creator>TOULEMONDE, Paul-Aymé</dc:creator>
<dc:creator>DIANI, Julie</dc:creator>
<dc:creator>GILORMINI, Pierre</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:description>The nonlinear behavior and failure of highly filled elastomers are significantly impacted by the volume fraction, the size and nature of fillers and the matrix stiffness. Original experimental data obtained on glass beads reinforced acrylates and on propellants allow illustrating and discussing the main effects generally observed.  In order to better understand the effects of the microstructure and constitutive parameters on the behavior and failure of highly filled elastomers,  a composite model, represented by a 2D periodic cell with randomly dispersed particles, with an account of a cohesive zone at the filler/matrix interface is used. Finite element simulations with finite strain provide insight on the stress-strain responses dependence to the model parameters and allow defining a failure criterion perceived by the appearance of a critical fibrillar microstructure.</dc:description>
</item>
<item>
<title>Roles of the Interphase Stiffness and Percolation on the Behavior of Solid Propellants</title>
<link>http://hdl.handle.net/10985/16018</link>
<description>Roles of the Interphase Stiffness and Percolation on the Behavior of Solid Propellants
TOULEMONDE, Paul-Ayme; DIANI, Julie; GILORMINI, Pierre; LACROIX, Geneviève; DESGARDIN, Nancy
Atomic force microscopy has provided access to local moduli for propellants prepared with bonding agents, which create a stiffness gradient in the matrix producing a stiffer interphase surrounding the fillers. The reinforcing impact of the bonding agent appears up to some distance and interphase percolation is observed. In order to better understand the impact of bonding agents on the stress and strain at break of propellants, finite element simulations are performed. Two-dimensional periodic cells containing randomly dispersed particles are considered, including both a cohesive zone model at the filler/matrix interface to account for possible debonding and an interphase that percolates or not. The influence of the interphase stiffness and of its percolation, on the stress and strain at break of the model propellants are evaluated through the use of a microstructure-based failure criterion.
</description>
<pubDate>Fri, 01 Jan 2016 00:00:00 GMT</pubDate>
<guid isPermaLink="false">http://hdl.handle.net/10985/16018</guid>
<dc:date>2016-01-01T00:00:00Z</dc:date>
<dc:creator>TOULEMONDE, Paul-Ayme</dc:creator>
<dc:creator>DIANI, Julie</dc:creator>
<dc:creator>GILORMINI, Pierre</dc:creator>
<dc:creator>LACROIX, Geneviève</dc:creator>
<dc:creator>DESGARDIN, Nancy</dc:creator>
<dc:description>Atomic force microscopy has provided access to local moduli for propellants prepared with bonding agents, which create a stiffness gradient in the matrix producing a stiffer interphase surrounding the fillers. The reinforcing impact of the bonding agent appears up to some distance and interphase percolation is observed. In order to better understand the impact of bonding agents on the stress and strain at break of propellants, finite element simulations are performed. Two-dimensional periodic cells containing randomly dispersed particles are considered, including both a cohesive zone model at the filler/matrix interface to account for possible debonding and an interphase that percolates or not. The influence of the interphase stiffness and of its percolation, on the stress and strain at break of the model propellants are evaluated through the use of a microstructure-based failure criterion.</dc:description>
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