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Studying Behavior of Paperboard Box: Experiment and Finite Element Model
Boussad Abbes,
Fazilay Abbes,
Lien Tien Dao,
Pham Tuong Minh Duong,
Viet Dung Luong
In the transportation and distribution of goods, cardboard boxes are often subjected to mechanical impacts such as shocks and random vibrations, which can cause damage to the goods. Many studies have focused on the durability of corrugated cardboard boxes. However, there is very limited research on compact cardboard boxes, especially in the case of exposure to random vibrations. In this study, static and dynamic tests on cardboard boxes were designed and conducted to determine compression strength, natural frequencies, and modal characteristics of the boxes. Subsequently, a finite element model of cardboard boxes taking into account the effects of the box manufacturing process on the mechanical properties of the cardboard, was developed to perform numerical simulations under compression and random vibrations. In this context, the in-plane orthotropic elastic-plastic behavior model of rigid cardboard was implemented in the Abaqus software through a VUMAT subroutine. Additionally, the parameters of the model were determined through an inverse identification process. Finally, numerical simulations of compression and random vibration tests were carried out to validate the experimental results. The comparison results show that the power spectral density (PSD) response of the mass/box system under random vibrations obtained through numerical simulations is consistent with the responses obtained from experimental measurements. Furthermore, the predicted force-displacement curves demonstrate good agreement with the measured curves.
In the transportation and distribution of goods, cardboard boxes are often subjected to mechanical impacts such as shocks and random vibrations, which can cause damage to the goods. Many studies have focused on the durability of corrugated cardboard boxes. However, there is very limited research on compact cardboard boxes, especially in the case of exposure to random vibrations. In this study, static and dynamic tests on cardboard boxes were designed and conducted to determine compression strength, natural frequencies, and modal characteristics of the boxes. Subsequently, a finite element model of cardboard boxes taking into account the effects of the box manufacturing process on the mechanical properties of the cardboard, was developed to perform numerical simulations under compression and random vibrations. In this context, the in-plane orthotropic elastic-plastic behavior model of rigid cardboard was implemented in the Abaqus software through a VUMAT subroutine. Additionally, the parameters of the model were determined through an inverse identification process. Finally, numerical simulations of compression and random vibration tests were carried out to validate the experimental results. The comparison results show that the power spectral density (PSD) response of the mass/box system under random vibrations obtained through numerical simulations is consistent with the responses obtained from experimental measurements. Furthermore, the predicted force-displacement curves demonstrate good agreement with the measured curves.
Posted: 14 March 2025
Analysis on Dynamic Tracking Characteristics of Dry Gas Seals During Start-up Process
Qiangguo Deng,
Yong Zhou,
Pingyang Yu,
Hengjie Xu,
Xuejian Sun,
Wenyuan Mao
Based on the small perturbation method, the transient pressure control equation considering real gas effects was solved, and the fitting expression for the dynamic characteristic parameters of the gas film during the start-up process was obtained. Subsequently, the influence of structural parameters of spiral groove dry gas seals on the dynamic tracking of the stationary ring's motion during the non-steady-state start-up process under three degree of freedom perturbations was analyzed. The results show that when the stationary and rotating rings initially separate, the stationary ring exhibits good tracking performance for both axial and angular motions of the rotating ring, although the tracking capability varies significantly. As time and film thickness increase, the tracking capability gradually weakens, and at the working film thickness, the tracking parameters tend to stabilize when the working film thickness is reached. Larger spiral angles and deeper dynamic pressure grooves, the poorer the axial and angular tracking performance of the sealing ring. The number of grooves has a minimal impact on the axial and angular tracking performance of the stationary ring. A higher balance coefficient improves the axial and angular tracking performance of the stationary ring.
Based on the small perturbation method, the transient pressure control equation considering real gas effects was solved, and the fitting expression for the dynamic characteristic parameters of the gas film during the start-up process was obtained. Subsequently, the influence of structural parameters of spiral groove dry gas seals on the dynamic tracking of the stationary ring's motion during the non-steady-state start-up process under three degree of freedom perturbations was analyzed. The results show that when the stationary and rotating rings initially separate, the stationary ring exhibits good tracking performance for both axial and angular motions of the rotating ring, although the tracking capability varies significantly. As time and film thickness increase, the tracking capability gradually weakens, and at the working film thickness, the tracking parameters tend to stabilize when the working film thickness is reached. Larger spiral angles and deeper dynamic pressure grooves, the poorer the axial and angular tracking performance of the sealing ring. The number of grooves has a minimal impact on the axial and angular tracking performance of the stationary ring. A higher balance coefficient improves the axial and angular tracking performance of the stationary ring.
Posted: 14 March 2025
Analytical Method of Sixth-Order Connecting Coupler-Curve Synthesis of Planar Four-Bar Linkages
Zhastalap Abilkaiyr,
Kuanysh Alipbayev,
Algazy Zhauyt,
Alisher Aden,
Yerbol Kaliyev,
Aray Orazaliyeva
Posted: 13 March 2025
Thermal Irreversibility in Nano-Enhanced Phase Change Material Liquefaction
Fikret Alic
Inside the closed, thin-walled hollow cylinder, there is a solid state of phase change material (NePCM) that has been nano-enhanced. This NePCM is heated at its bottom. Nanoparticles (Al2O3) were inserted and homogenized within the PCM (sodium acetate trihydrate, C2H3O2Na), to create the NePCM. The hollow cylinder is thermally insulated from the outside ambient temperature, while the heat supplied is enough to cause a phase change. Once the entire NePCM has converted from a solid to a liquid due to heating, it is then cooled, and the thermal insulation is removed. The cylindrical liquefied NePCM bar is cooled in this manner. Thermal entropy, entransy dissipation rate, and bar efficiency during the heating and cooling of NePCM bar were analyzed by changing variables. The volume fraction ratio of nanoparticles, inlet heat flux, and liquefied bar height were the variables considered. The results indicate a significant impact on the NePCM bar during liquefaction and convective cooling when the values of these variables are altered. For instance, with an increase in the volume fraction ratio from 3% to 9%, at a constant heat flux of 104 Wm-2 and a liquefied bar height of 0.02m, the NePCM bar efficiency decreases to 99%. The thermal entropy from heat conduction through liquefied NePCM bar is significantly lower compared to thermal entropy from convective air cooling on its surface. The thermal entropy of the liquefied NePCM bar increases on average by 110% without any cooling. With a volume fraction ratio of 6%, there is an 80% increase in heat flux as the bar height increases to 0.02m.
Inside the closed, thin-walled hollow cylinder, there is a solid state of phase change material (NePCM) that has been nano-enhanced. This NePCM is heated at its bottom. Nanoparticles (Al2O3) were inserted and homogenized within the PCM (sodium acetate trihydrate, C2H3O2Na), to create the NePCM. The hollow cylinder is thermally insulated from the outside ambient temperature, while the heat supplied is enough to cause a phase change. Once the entire NePCM has converted from a solid to a liquid due to heating, it is then cooled, and the thermal insulation is removed. The cylindrical liquefied NePCM bar is cooled in this manner. Thermal entropy, entransy dissipation rate, and bar efficiency during the heating and cooling of NePCM bar were analyzed by changing variables. The volume fraction ratio of nanoparticles, inlet heat flux, and liquefied bar height were the variables considered. The results indicate a significant impact on the NePCM bar during liquefaction and convective cooling when the values of these variables are altered. For instance, with an increase in the volume fraction ratio from 3% to 9%, at a constant heat flux of 104 Wm-2 and a liquefied bar height of 0.02m, the NePCM bar efficiency decreases to 99%. The thermal entropy from heat conduction through liquefied NePCM bar is significantly lower compared to thermal entropy from convective air cooling on its surface. The thermal entropy of the liquefied NePCM bar increases on average by 110% without any cooling. With a volume fraction ratio of 6%, there is an 80% increase in heat flux as the bar height increases to 0.02m.
Posted: 13 March 2025
Parameters Optimization of Orbital TIG Welding on the Stainless Steel Pipe
Ngoc-Thien Tran,
Van-Thuc Nguyen
Orbital TIG welding is widely applied to weld pipes to pipes in many fields, such as food, chemical, oil, gas, and transportation. Optimizing welding parameters such as voltage, current, and travel speed is critical to achieve a good quality weld. This study investigates the impacts of orbital welding parameters and filler wire diameters on the tensile strength of 304 stainless steel pipes. The 304 stainless steel pipe has an outer diameter of 76 mm and a thickness of 2 mm. Filler wire is used with the workpiece and is available in three diameters of 0.8 mm, 1 mm, and 1.2 mm; wire feed speed from 3.8 mm/s to 5.6 mm/s; current from 90 A to 110 A; travel speed is fixed at 5.5 mm/s. The highest tensile strength of 562 Mpa is achieved with the heat input of 0.32 KJ/mm and wire feed speed of 3.8 mm/s. In addition, the best parameters via the Taguchi method were found. The parameters’ influence trends on the weld quality were also revealed.
Orbital TIG welding is widely applied to weld pipes to pipes in many fields, such as food, chemical, oil, gas, and transportation. Optimizing welding parameters such as voltage, current, and travel speed is critical to achieve a good quality weld. This study investigates the impacts of orbital welding parameters and filler wire diameters on the tensile strength of 304 stainless steel pipes. The 304 stainless steel pipe has an outer diameter of 76 mm and a thickness of 2 mm. Filler wire is used with the workpiece and is available in three diameters of 0.8 mm, 1 mm, and 1.2 mm; wire feed speed from 3.8 mm/s to 5.6 mm/s; current from 90 A to 110 A; travel speed is fixed at 5.5 mm/s. The highest tensile strength of 562 Mpa is achieved with the heat input of 0.32 KJ/mm and wire feed speed of 3.8 mm/s. In addition, the best parameters via the Taguchi method were found. The parameters’ influence trends on the weld quality were also revealed.
Posted: 13 March 2025
Assessing the Meshing for Windage Power Losses Simulation of an Orthogonal Face Gear
Tiberiu-Daniel Pau,
Zoltan-Iosif Korka,
Dorian Nedelcu,
Corneliu HRIMIUC
Posted: 12 March 2025
Application of Machine Learning in Predicting Quality Parameters in Metal Material Extrusion (MEX/M)
Karim Asami,
Maxim Kühne,
Tim Röver,
Claus Emmelmann
Posted: 11 March 2025
Optimal Design Methodology of Maxwell Coulomb Friction Damper
Chun Nam Wong,
Wai On Wong
An optimal design methodology of Maxwell Coulomb friction damper is proposed for minimization of resonant vibration of dynamic structures. The simple Coulomb friction damper has the problem of zero or little damping effect to the vibration of spring-mass dynamic system at resonance. This problem does not exist in the case of Maxwell Coulomb friction damper which can be formed by combining a Coulomb friction damper with a spring element in series. However, the design and analysis of Maxwell Coulomb friction damper is more complicated and an optimal design methodology of such nonlinear damper is proposed in this article. The nonlinear equations of motion of the proposed damper is modelled and its hysteresis loop can be constructed by combining the four different cases of stick-slide motion. Its nonlinear equations of motion are solved numerically and the optimal values of friction and stiffness of the proposed damper is determined by using a Newton search method. Experimental validation of the optimal design of Maxwell Coulomb friction damper is carried out with a prototype of the proposed damper mounted on a linear slide block platform. Close correlation with its numerical predictions is observed in its contour plot of resonant vibration amplitude of the primary system. Damping performance of proposed damper is compared to viscous damper in seismic response design of adjacent single-storey buildings and also for damping turbine blade vibrations.
An optimal design methodology of Maxwell Coulomb friction damper is proposed for minimization of resonant vibration of dynamic structures. The simple Coulomb friction damper has the problem of zero or little damping effect to the vibration of spring-mass dynamic system at resonance. This problem does not exist in the case of Maxwell Coulomb friction damper which can be formed by combining a Coulomb friction damper with a spring element in series. However, the design and analysis of Maxwell Coulomb friction damper is more complicated and an optimal design methodology of such nonlinear damper is proposed in this article. The nonlinear equations of motion of the proposed damper is modelled and its hysteresis loop can be constructed by combining the four different cases of stick-slide motion. Its nonlinear equations of motion are solved numerically and the optimal values of friction and stiffness of the proposed damper is determined by using a Newton search method. Experimental validation of the optimal design of Maxwell Coulomb friction damper is carried out with a prototype of the proposed damper mounted on a linear slide block platform. Close correlation with its numerical predictions is observed in its contour plot of resonant vibration amplitude of the primary system. Damping performance of proposed damper is compared to viscous damper in seismic response design of adjacent single-storey buildings and also for damping turbine blade vibrations.
Posted: 11 March 2025
Stall Characteristics in a Transonic Axial Compressor with Self-Recirculating Flow Control
Darius V Ahmadi,
Walter C Smith,
Anthony J Gannon,
Garth V Hobson
Posted: 11 March 2025
Insight Into the Impact of Blade Perforation on the Aerodynamics and Acoustics of a Two-Stage Variable-Pitch Axial Fan
Chen Qiao,
Xuemin Ye,
Yunhao Wu,
Chunxi Li
Posted: 10 March 2025
Enhancing Precision in Arc Welding Simulations: A Comprehensive Study on Ellipsoidal Heat Source Model
Ergün Nart,
Senol Sert
Arc welding is a complex multi-physics process, and its finite element simulation requires significant computational resources to determine temperature distributions in engineering problems accurately. Engineers and researchers aim to achieve reliable results from finite element analysis while minimizing computational costs. This research extensively studies the application of conventional ellipsoidal heat source formulation to obtain improved temperature distribution during arc welding for practical applications. Approximated ellipsoidal heat source model, which artificially modifies the coefficient of thermal conductivity in the welding pool area to simulate stirring effects, (Modified Ellipsoidal Model) is shown to be scientifically valid by comparing its results with those of Comsol's multi-physics arc welding models. The results show that, in comparison to the conventional ellipsoidal model, the temperature distributions obtained using the modified ellipsoidal model closely approach those from multi-physics simulations. In particular, the temperature history in the middle of the weld pool significantly changes and approaches the multiphysics solutions. Additionally, several points near the heat-affected zone were analyzed, and both ellipsoidal methods produced similar temperature histories until the metal melted. After melting, the modified ellipsoidal method gradually aligns more closely with the multiphysics solution. Additionally, both ellipsoidal methods produce similar temperature histories at points within the heat-affected zone.
Arc welding is a complex multi-physics process, and its finite element simulation requires significant computational resources to determine temperature distributions in engineering problems accurately. Engineers and researchers aim to achieve reliable results from finite element analysis while minimizing computational costs. This research extensively studies the application of conventional ellipsoidal heat source formulation to obtain improved temperature distribution during arc welding for practical applications. Approximated ellipsoidal heat source model, which artificially modifies the coefficient of thermal conductivity in the welding pool area to simulate stirring effects, (Modified Ellipsoidal Model) is shown to be scientifically valid by comparing its results with those of Comsol's multi-physics arc welding models. The results show that, in comparison to the conventional ellipsoidal model, the temperature distributions obtained using the modified ellipsoidal model closely approach those from multi-physics simulations. In particular, the temperature history in the middle of the weld pool significantly changes and approaches the multiphysics solutions. Additionally, several points near the heat-affected zone were analyzed, and both ellipsoidal methods produced similar temperature histories until the metal melted. After melting, the modified ellipsoidal method gradually aligns more closely with the multiphysics solution. Additionally, both ellipsoidal methods produce similar temperature histories at points within the heat-affected zone.
Posted: 10 March 2025
Effect of Varying Layer Thickness by Interlayer Machining on Microstructure and Mechanical Properties in Wire Arc Additive Manufacturing
Ganesan G.,
Neel Kamal Gupta,
Siddhartha S.,
Shahu R. Karade,
Henning Zeidler,
Narasimhan Krishnaiyengari,
Karunakaran K. P.
This study focuses on how varying layer thickness by interlayer machining affects microstructure refinement, mechanical properties, and residual stresses of Wire Arc Additive Manufacturing (WAAM) components. It compares four types of WAAM samples: As built with uneven layer thickness without interlayer machining and uniform layer thicknesses of 2mm, 1.5mm, and 1mm achieved through interlayer machining. It reveals that the machining force reduces grain size and residual stress in WAAM components. Moreover, uniform and smaller layer thickness enhances inter-layer bonding, improving mechanical properties but increases the build time with more layers of deposition.
This study focuses on how varying layer thickness by interlayer machining affects microstructure refinement, mechanical properties, and residual stresses of Wire Arc Additive Manufacturing (WAAM) components. It compares four types of WAAM samples: As built with uneven layer thickness without interlayer machining and uniform layer thicknesses of 2mm, 1.5mm, and 1mm achieved through interlayer machining. It reveals that the machining force reduces grain size and residual stress in WAAM components. Moreover, uniform and smaller layer thickness enhances inter-layer bonding, improving mechanical properties but increases the build time with more layers of deposition.
Posted: 10 March 2025
Structural Design and Random Vibration Analysis of a High-Stability Momentum Wheel
Yukuan Xie,
Yuan Xue,
Hongxiang Wang,
Yinjin Sun
Posted: 10 March 2025
Acceleration Energies and Higher-Order Dynamic Equations in Analytical Mechanics
Iuliu Negrean,
Adina Veronica Crișan,
Sorin Vlase
The dynamic study of current and rapid movements of rigid and multibody mechanical systems, according to differential principles from dynamics, is based on advanced concepts from analytical mechanics: kinetic energy, higher-order acceleration energies and their absolute time derivatives. In advanced dynamics, the study will extend to higher-order acceleration energies. This paper, reflecting the authors’ research, presents new and revised formulations in advanced kinematics and dynamics, with a focus on acceleration energies of higher order. Explicit and matrix representations of the defining expressions for higher-order acceleration energies, relevant to the current and rapid movements of rigid bodies and multibody mechanical systems, will be presented. These formulations include higher-order absolute time derivatives of advanced concepts, following the specific equations from analytical dynamics. Based on authors’ findings, acceleration energies play a central, decisive role in formulating higher-order differential equations, which describe both rapid and transient motion behavior in rigid and multibody systems.
The dynamic study of current and rapid movements of rigid and multibody mechanical systems, according to differential principles from dynamics, is based on advanced concepts from analytical mechanics: kinetic energy, higher-order acceleration energies and their absolute time derivatives. In advanced dynamics, the study will extend to higher-order acceleration energies. This paper, reflecting the authors’ research, presents new and revised formulations in advanced kinematics and dynamics, with a focus on acceleration energies of higher order. Explicit and matrix representations of the defining expressions for higher-order acceleration energies, relevant to the current and rapid movements of rigid bodies and multibody mechanical systems, will be presented. These formulations include higher-order absolute time derivatives of advanced concepts, following the specific equations from analytical dynamics. Based on authors’ findings, acceleration energies play a central, decisive role in formulating higher-order differential equations, which describe both rapid and transient motion behavior in rigid and multibody systems.
Posted: 07 March 2025
A Comprehensive Review of Curved Shell Structures Against Buckling Failures
Mohd Shahrom Ismail,
Jamaluddin Mahmud,
Olawale Ifayefunmi,
Judha Purbolaksono
Posted: 06 March 2025
Analysis of Pressure Pulsations in Variable Flow Axial Piston Pumps in Hydraulic Installations of Agricultural Machinery
Andrzej Banaszek,
Maja Andjelković,
Radovan Petrović,
Slavica R. Mihajlović,
Nataša Djordjević,
Jasmina Lozanović
Posted: 05 March 2025
Influence of Inner Lining Atoms of Multilayered Hexagonal Boron Nitride Porous Membrane on Desalination
Chulwoo Park,
Daejoong Kim
Posted: 05 March 2025
Experimental Study and Numerical Simulation for Sediment’s Promoting Effect on Cavitation Based on Flow Field Analysis
Zeyuan Yang,
Qin Zhao,
Gang Yu
Posted: 05 March 2025
Comparative Study of a 2-DoF Hybrid Piezoelectric-Electromagnetic Energy Harvester and a Standalone Piezoelectric Harvester
Issam M. Bahadur,
Hassen Ouakad,
El Manaa Barhoumi,
Asan Muthalif,
Muhammad Hafizh,
Jamil Renno,
Mohammad Paurobally
Posted: 05 March 2025
Theoretical and Numerical Research on High-Speed Small Refrigeration Twin-Screw Compressor
Kai Ma,
Xiaokun Wu,
Huaican Liu,
Dantong Li,
Zhilong He
To investigate the performance of high-speed miniaturized screw refrigeration compressors, this study designed rotors with identical theoretical displacement but varying rated speeds. A normalized analysis established quantitative evaluation criteria for geometric performance, while an exergy analysis model assessed leakage exergy losses. Thermodynamic modeling evaluated the impact of different clearances and rated speeds on performance. The computational fluid dynamics (CFD) simulations analyzed gas forces and torque acting on the rotors. The study reveals that while tooth tip leakage represents the largest volumetric leakage in screw compressors, contact line leakage contributes most significantly to power losses. When the rated speed increases from 3000 rpm to 15000 rpm, contact line leakage remains the dominant source of power loss, with its relative contribution showing a marked increase. The rate of efficiency improvement with increasing speed follows a non-linear relationship, demonstrating diminishing returns at ultra-high speeds where further speed elevation provides negligible efficiency gains. For compressors with identical cylinder dimensions, reducing the number of lobes decreases discharge pressure fluctuations and power consumption. Larger wrap angles increase contact line length and discharge port area, reducing volumetric efficiency while creating a trade-off between leakage and discharge losses, resulting in an optimal wrap angle that maximizes adiabatic efficiency.
To investigate the performance of high-speed miniaturized screw refrigeration compressors, this study designed rotors with identical theoretical displacement but varying rated speeds. A normalized analysis established quantitative evaluation criteria for geometric performance, while an exergy analysis model assessed leakage exergy losses. Thermodynamic modeling evaluated the impact of different clearances and rated speeds on performance. The computational fluid dynamics (CFD) simulations analyzed gas forces and torque acting on the rotors. The study reveals that while tooth tip leakage represents the largest volumetric leakage in screw compressors, contact line leakage contributes most significantly to power losses. When the rated speed increases from 3000 rpm to 15000 rpm, contact line leakage remains the dominant source of power loss, with its relative contribution showing a marked increase. The rate of efficiency improvement with increasing speed follows a non-linear relationship, demonstrating diminishing returns at ultra-high speeds where further speed elevation provides negligible efficiency gains. For compressors with identical cylinder dimensions, reducing the number of lobes decreases discharge pressure fluctuations and power consumption. Larger wrap angles increase contact line length and discharge port area, reducing volumetric efficiency while creating a trade-off between leakage and discharge losses, resulting in an optimal wrap angle that maximizes adiabatic efficiency.
Posted: 04 March 2025
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