Applied sciences

Archive of Mechanical Engineering

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Archive of Mechanical Engineering | 2025 | vol. 72 | No 4

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Abstract

This paper presents a numerical investigation of unsteady, two-dimensional magnetohydrodynamic (MHD) mixed convection flow and heat transfer over a permeable stretching cylinder embedded in a porous medium. The governing conservation equations of mass, momentum, and energy are formulated by incorporating the effects of viscous dissipation, temperature-dependent thermal conductivity, Joule heating, thermal radiation, and a uniform transverse magnetic field (with negligible induced effects). Additionally, slip velocity and variable surface heat flux are also considered to enhance the model’s applicability to engineering systems. Through appropriate similarity transformations, the governing partial differential equations are reduced to a set of nonlinear ordinary differential equations, which are solved using MATLAB’s bvp4c scheme. The influence of key dimensionless parameters on velocity and temperature distributions, skin friction coefficient, and Nusselt number is thoroughly examined. Comparative analysis between the stretching cylinder and the flat sheet configurations reveals that the cylinder’s curvature significantly thickens the momentum and thermal boundary layers, while enhancing the surface shear stress and heat transfer rate. These findings offer useful implications for the design of thermal systems involving curved geometries, such as cylindrical heat exchangers and pipes.
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Authors and Affiliations

Shubham Bansal
1 2
ORCID: ORCID
Rajendra Singh Yadav
1
Ankita Ankita
3
ORCID: ORCID
Oluwole Daniel Makinde
4

  1. Department of Mathematics, University of Rajasthan, Jaipur, Rajasthan-302004, India
  2. SBD Government College, Sardarshahar, Churu, Rajasthan-331403, India
  3. Department of Physics, Government Girls College, Taranagar, Rajasthan-331304, India
  4. Faculty of Military Science, Stellenbosch University, Saldanha, South Africa
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Abstract

The modern battlefield requires highly accurate missiles, which has led to the modification of unguided missiles into guided versions. This paper presents the process of adapting an unguided missile with a range of 40 km into a guided version using a canard control system. A key aspect of the upgrade was the development of a control system that allows the trajectory to be corrected after crossing the apex of the flight path, particularly during the descent phase. This paper discusses the design details and application of a two-channel control system (pitch and yaw) in which the control signals are synchronized with the speed of the projectile. Mathematical modelling and numerical simulations have shown that, with appropriate control parameters, a zero mean control force can be achieved, leading to trajectory stabilization and minimized aiming errors. The proposed solution provides a basis for further research and dynamic field tests and can contribute to the development of precision guidance technology for surface-to-surface missiles.
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Authors and Affiliations

Adrian Szklarski
1
ORCID: ORCID
Robert Głębocki
2
ORCID: ORCID

  1. Division of Automation and Aeronautical Systems, Faculty of Power and Aeronautical Engineering, Warsaw University of Technology, Poland
  2. Division of Mechanics, Faculty of Power and Aeronautical Engineering, Warsaw University of Technology, Poland
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Abstract

Fuel tanks in vehicles traveling in danger zones are susceptible to damage resulting from shelling. Ensuring adequate strength of this type of construction elements is extremely important. The object of the research was a fuel tank from a leading manufacturer, declared as made of an external coating that allows for closing gunshot holes. The tank was subjected to fire in two variants: without additional protection and with additional protection in the form of Armox 500T armor plate with a thickness of 4.5 mm. Additionally, the authors also performed numerical analyzes in the Abaqus/Explicit program, which were used to reproduce the physical phenomena occurring during shooting. The developed geometric models and the declared initial boundary conditions reflected the actual test conditions, and the Johnson-Cook model and the failure model were used. These tests assessed the tank's resistance to shooting, the extent to which the gunshot holes closed and the possibility of fuel ignition inside the tank. Then, verification tests were carried out in which 4 mm sheet metal panels were shot at to validate the numerical results for the adopted material model of the shield. The obtained results from numerical simulations corresponded appropriately with the results of experiments. Building upon this correspondence, the study offers an innovative contribution by integrating a comprehensive ballistic evaluation of a real, self-sealing fuel tank system with detailed numerical validation based on advanced material failure modelling and parameter sensitivity analysis. The results obtained may serve as a reference for the design and optimization of protective systems in armored vehicles, particularly regarding enhancing fuel system survivability under ballistic impact.
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Authors and Affiliations

Maciej Roszak
1
ORCID: ORCID
Dariusz Pyka
1
ORCID: ORCID
Maksymilian Stępczak
1
ORCID: ORCID
Paweł Sweklej
2
ORCID: ORCID
Krzysztof Jambroziak
1
ORCID: ORCID
Mirosław Bocian
1
ORCID: ORCID

  1. Department of Mechanics, Materials and Biomedical Engineering, Wrocław University of Science and Technology, Wrocław, Poland
  2. Military Institute of Armament Technology, Zielonka, Poland
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Abstract

Lightweight sandwich structures with honeycomb cores represent a critical advancement in engineering design, offering superior strength-to-weight ratios crucial for aerospace, marine, and civil applications. While extensive research exists on flows past isotropic rectangular cylinders, the fluid-structure interaction (FSI) behavior of orthotropic honeycomb structures remains poorly understood. This study investigates how the orthotropic characteristics of honeycomb sandwich panels affect their structural responses under fluid loading conditions. Using ANSYS CFX, we conducted three-dimensional finite volume simulations with one-way FSI coupling at Reynolds numbers ranging from 5x104 to 2.5x105. The computational domain was validated through mesh convergence studies and compared against existing experimental data for rectangular cylinders. Two cases were analyzed: honeycomb sandwich panels and equivalent-weight flat panels, both subjected to identical flow conditions. Results demonstrate that honeycomb panels exhibit superior performance, tolerating 17% higher pressure loads while showing 28% less deformation compared to flat panels. This enhanced structural efficiency is attributed to the honeycomb core's ability to distribute loads more effectively through its cellular structure. Our findings provide quantitative guidance for designing honeycomb sandwich panels in fluid-loaded applications, particularly in marine and aerospace environments where structural efficiency is paramount.
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Authors and Affiliations

Fatemeh Asadi Talebbeigi
1
ORCID: ORCID
Saeed Jamei
2
ORCID: ORCID
Mohammad Amin Esabat
2
ORCID: ORCID

  1. Ocean Engineering Department, Texas A&M University, Galveston, USA
  2. Department of Marine Engineering, Faculty of Engineering, Persian Gulf University, Bushehr, Iran
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Abstract

This article presents the results obtained in the multibody dynamics model of the cycloidal gearbox with Hunt and Crossley contact modelling. The model is implemented in Fortran and uses the 2nd order Runge-Kutta method to integrate the motion equations. The contact modelling requires discretization of the cycloidal wheel profile. In previous models, the discretization has been performed using constant increments in the parameter of the cycloidal wheel equations. The presented version of the model uses uniform discretization of the cycloidal wheel, which is implemented using arc length calculation, bisection method and derivatives of the profile. The results show that the numerical solution of derivatives is the main issue in the model with uniform discretization. When the contact point lies near the inflection point of the cycloid, the radius of curvature tends to be infinite. The previous model, which used parameter discretization and calculated curvature based on the radius of a circle passing through three neighboring points on the cycloidal wheel, exhibited lower numerical errors and smoother time profiles of the dynamic variables. Despite the expectations that equal discretization would provide better energy stability, it turned out that the use of parametric discretization is simpler and more reliable.
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Authors and Affiliations

Roman Król
1
ORCID: ORCID

  1. Casimir Pulaski Radom University, Radom, Poland
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Abstract

The paper describes the model of an oscillator with damping, whose vibrations are forced by a random series of impulses. The mathematical model of the inverse problem used to calculate the distributions can only be applied when the values of the random impulses are known. If impulse values cannot be estimated based on the vibration signal, machine learning algorithms and feature engineering should be used to determine their distribution. In the discussed paper, unsupervised machine learning (specifically, the agglomerative hierarchical clustering) is employed to evaluate the applicability of the algorithms to the problem of recognizing the magnitudes of random impulses and characterizing their distributions.
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Authors and Affiliations

Natalia Frankowska
1
ORCID: ORCID
Agnieszka Ozga
1

  1. AGH University of Krakow, Krakow, Poland
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Abstract

The automatic conveying line is the key equipment of material flow system in logistics distribution centers. However, conventional automatic conveying line would take up a relatively large place, yet it could only perform simple tasks such as moving packages along a straight line. It is also difficult and costly to add/change an existing conveying line, which makes the distribution center rigid, inflexible, and unfriendly to maintain. To improve the automatic conveying line, this paper proposed a roller array-based package transport and sorting platform, which can be used for logistics distribution centers for advanced automatic conveying purposes. The roller unit is the key component of the platform. It consists of a swiveling roller and a swiveling motor which give the packages the required direction and velocity. Package detection technique is also integrated in the platform to detect the geometry center of the moving package for transport feedback control. The proposed control algorithm enables the platform to perform package translation, rotation, turning and a normal transport. The experiment results show that the transport velocity error is about 6% and the rotation angular velocity error is 5%. The package could move along the designed ‘S’ shape trajectory. The proposed roller array-based package transport and sorting platform could control the package movement as required.
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Authors and Affiliations

Ruipeng Li
1
ORCID: ORCID
Miaocan Hu
1
ORCID: ORCID
Shuangying Pan
2
ORCID: ORCID
Xiang Lou
1
ORCID: ORCID
Qihua Yang
1

  1. College of Mechanical and Electrical Engineering, China Jiliang University, Hangzhou, China
  2. HangZhou WREN Hydraulic Equipment Manufacturing Co.,Ltd, Hangzhou, China