Vojnotehnički glasnik / Military Technical Courier https://www.aseestant.ceon.rs/index.php/vtg <p>The <em>Military Technical Courier</em> is a multidisciplinary scientific journal of the Ministry of Defence and the Serbian Armed Forces. The publisher of the journal is the University of Defence in Belgrade. The journal publishes scientific and professional papers covering fundamental research (mathematics, computer science and mechanics) and technological development (electronics, telecommunications, information technologies, mechanical engineering, material science and chemical technologies) as well as technical data on modern weapon systems and military technologies.</p> University of Defence in Belgrade sr-RS@latin Vojnotehnički glasnik / Military Technical Courier 0042-8469 <h3>Proposed Creative Commons Copyright Notices</h3> <h4>Proposed Policy for Military Technical Courier (Journals That Offer Open Access)</h4> <p>Authors who publish with this journal agree to the following terms:<br>Authors retain copyright and grant the journal right of first publication with the work simultaneously licensed under a <a href="http://creativecommons.org/licenses/by/3.0/" target="_new"><span style="color: #2e526d;">Creative Commons Attribution License</span></a> that allows others to share the work with an acknowledgement of the work's authorship and initial publication in this journal.</p> <ol type="a"> <li class="show">Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the journal's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgement of its initial publication in this journal.</li> <li class="show">Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See <a href="http://opcit.eprints.org/oacitation-biblio.html" target="_new"><span style="color: #2e526d;">The Effect of Open Access</span></a>).</li> </ol> Front impressum for the issue 1-2026 https://www.aseestant.ceon.rs/index.php/vtg/article/view/65825 Vladan Anicijevic Copyright (c) 2026 Vladan Anicijevic https://creativecommons.org/licenses/by/4.0 2026-03-18 2026-03-18 74 1 10.5937/vojtehg74-65825 Contents for the issue 1-2026 https://www.aseestant.ceon.rs/index.php/vtg/article/view/65827 Vladan Anicijevic Copyright (c) 2026 Vladan Anicijevic https://creativecommons.org/licenses/by/4.0 2026-03-18 2026-03-18 74 1 10.5937/vojtehg74-65827 Sustainable fibre-concrete reinforcement using manufacturing by-products https://www.aseestant.ceon.rs/index.php/vtg/article/view/58016 <p class="S06bTekstsaetkanapoetkulanka" style="text-align: justify;"><span lang="sr">Introduction/purpose: Concrete is a material with very high compressive strength compared to very low tensile strength, which makes it brittle when subjected to tensile and bending stresses, with premature failure manifested by cracking. These stresses can be improved by reinforcing concrete with different types of fibres derived from industrial or other wastes.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Methods: In this context, this work aims to use industrial metal waste in concrete and compare it with metal fibre concrete to overcome this tensile strength deficiency. Two types of industrial fibres and two other types of waste were used, aluminium and steel waste (in the form of shavings) re</span><span lang="EN-GB" style="mso-ansi-language: EN-GB;">covered from mechanical milling plants. The properties of the different </span><span lang="sr">fibre concretes in the fresh and hardened states are analysed and compa</span><span lang="EN-GB" style="mso-ansi-language: EN-GB;">red with natural non-fibre concrete.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Results: The experimental results suggest that incorporating such waste in concrete reduces the workability of concrete mixtures, improves the tensile strength of concrete, and reduces considerably its shrinkage without affecting its compressive strength.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-bottom: 0.0001pt; text-align: justify;"><span lang="EN-GB" style="mso-ansi-language: EN-GB;">Conclusion: Following a rigorous analysis of the obtained results, it was determined that the optimum percentage of recycled fibre in steel is 15%. The tensile strength at this level is comparable to that of industrial fibre-reinforced concrete. This finding is very relevant to the sustainable development strategy of the Algerian government, which promotes the improvement of characteristics and the conservation of natural resources.</span></p> Ilyes IRKI Mohamed KESSEIR Farid DEBIEB Chafika SETTARI Copyright (c) 2026 Ilyes IRKI, Mohamed KESSEIR, Farid DEBIEB , Chafika SETTARI https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 225 243 10.5937/vojtehg74-58016 Selection of 3D Printer for racing car spoilers using Entropy - CRADIS model https://www.aseestant.ceon.rs/index.php/vtg/article/view/58269 <p class="S06bAbstracttextatthebeginningofthearticle"><span lang="sr">Introduction/purpose: This study aims to identify the most suitable 3D printer for manufacturing racing car spoilers.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle"><span lang="sr">Methods: </span><span lang="EN-US" style="mso-ansi-language: EN-US;">Sixteen different 3D printing machines are evaluated based on eight selection criteria. The criteria weights are determined using the Entropy method, while Compromise Ranking of Alternatives from Distance to Ideal Solution (CRADIS) method is applied to rank the machines and identify the best option for spoiler production. Sensitivity analysis is conducted using various methods to validate the results.<span style="mso-spacerun: yes;">&nbsp; </span></span></p> <p class="S06bAbstracttextatthebeginningofthearticle"><span lang="sr">Results: Ultimaker 2 is identified as the most suitable 3D printer, followed by Delta Non-Turbo WASP 2040, while UP Plus 2 ranks as the least favorable.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-bottom: .0001pt;"><span lang="sr">Conclusion: By using the Entropy and CRADIS method</span><span lang="sr" style="color: windowtext;">, </span><span lang="EN-US" style="color: windowtext; mso-ansi-language: EN-US;">Ultimaker 2, is identified as the best-performing 3D printer, followed by <a name="_Hlk192590249"></a>Delta Non-Turbo WASP 2040, while UP Plus 2 received the lowest ranking. Various MCDM methods are applied for performance comparison and sensitivity analysis, with the Spearman Rank Correlation Coefficient applied to assess the correlation between different MCDM methods</span><span lang="sr" style="color: windowtext;">.</span></p> Rajeev Ranjan Sonu Rajak Prasenjit Chatterjee Copyright (c) 2026 Rajeev Ranjan, Sonu Rajak, PRASENJIT CHATTERJEE https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 50 79 10.5937/vojtehg74-58269 Comprehensive study of the effect of a structural parameter of hydraulic buffer on the firing stability of grenade launchers https://www.aseestant.ceon.rs/index.php/vtg/article/view/58331 <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;">Introduction/purpose: The article's main goal is to present a novel method for evaluating the stability of automatic weapons mounted on tripods when firing in series.</p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;">Methods: The mathematical model is established based on the theory of many-body mechanics. The Lagrange II equation is used to establish the system of differential equations of motion of mechanical system. The mathematical model considers the influence of the ground elasticity and the impact of the gunner through elastic-damping connections. Dynamic simulations were performed on the AGS-17 grenade launcher. The calculated results were then compared with the experimental results to verify the proposed model.</p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;">Results: The comparison results show an unexpected confidence level between the theoretical model and experimental results. The errors in muzzle velocity and firing rate are 2.52% and 6.18%, respectively. Based on the theoretical basis of the mathematical model, the influence of some structural parameters of the hydraulic buffer on the firing stability of the automatic grenade launcher was investigated. The research results provide a reliable theoretical basis to improve, design, and manufacture hydraulic buffers for grenade launchers in particular and automatic guns in general.</p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;">Conclusion: The research results presented in this paper ensure high accuracy and reliability. This paper provides a reliable scientific document for the optimal design of the overall structure of the weapon system.</p> Dung Nguyen Van Vo Van Bien Phu Nguyen Minh Hung Dao Manh Copyright (c) 2026 Dung Nguyen Van, Vo Van Bien, Phu Nguyen Minh, Hung Dao Manh https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 80 103 10.5937/vojtehg74-58331 Laser obscuration and infrared emission characteristics of red phosphorus and mg-al based smoke composition https://www.aseestant.ceon.rs/index.php/vtg/article/view/58344 <p class="S06bTekstsaetkanapoetkulanka" style="text-align: justify;"><span lang="sr">Introduction/purpose: The capability for laser attenuation and infrared (IR) radiation emission is one of the most essential characteristics determining the camouflage effectiveness of multispectral smoke screens on the battlefield. In this study, the effects of red phosphorus and Mg-Al content, the initial mass of the smoke composition, and the relative humidity on the obscuration characteristics of smoke cloud, including the degree of laser attenuation, the mass extinction coefficient, the Yield factor, and the Figure of Merit, were examined. Additionally, the IR emission properties of smoke screens based on RP/Mg-Al were also evaluated. </span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Methods: Laser radiation attenuation was evaluated by comparing the initial laser power to the power measured after passing through the smoke screen. A 1.064 &micro;m, 11.0 mW continuous-wave laser was transmitted through the test chamber and measured with a power meter. The infrared properties of the smoke clouds were analyzed using an SR-5000N spectral radiometer within the 2.5 &ndash; 14.0 &micro;m range. </span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Results: The results indicate that increasing the content of red phosphorus, sample masses, and relative humidity enhances the laser obscuration characteristics. Notably, for a 1 m<sup>3</sup> smoke chamber, the estimated optimal sample masses are 3.25 g and 2.30 g at 65% and 90% relative humidity, respectively. Furthermore, increasing Mg-Al content enhances IR emission in the &beta; band (3-5 &mu;m), while emission in the &gamma; band (8-14 &mu;m) decreased.<span style="mso-spacerun: yes;">&nbsp;&nbsp; </span></span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Conclusion: The laser obscuration characteristics of RP/Mg-Al-based smoke compositions can be effectively controlled by optimizing the RP/Mg-Al content and relative humidity levels. Moreover, the RP/Mg-Al-based compositions demonstrate strong IR radiation characteristics, which are also influenced by the content of RP and Mg-Al. Future research should focus on evaluating the obscuration characteristics of RP/Mg-Al-based compositions in the near- and far-IR regions.</span></p> Dinh Thang Pham Duc Nhan Phan Trung Toan Nguyen Copyright (c) 2026 Dinh Thang Pham, Duc Nhan Phan, Trung Toan Nguyen https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 208 224 10.5937/vojtehg74-58344 Some considerations on thermodynamics of quantum mechanics on a circle and Kałuża–Klein models https://www.aseestant.ceon.rs/index.php/vtg/article/view/58405 <p class="MsoNormal" style="text-align: justify;">Introduction/purpose: Quantum mechanics on a circle has been investigated and applied to a Kałuża&ndash;Klein model with a compactified dimension.</p> <p class="MsoNormal" style="text-align: justify;">Methods: Methods of quantum mechanics and statistical mechanics were employed. Additionally, a Kałuża&ndash;Klein toy model with compactified dimension was considered.</p> <p class="MsoNormal" style="text-align: justify;">Results: The resulting partition function can be evaluated in a closed form, giving a special function. It presents a phase transition depending on the geometry. When used in a Kałuża&ndash;Klein model, it showed a phase transition regulated by the radius of the circle, and the transition disappears when the radius is infinite, that is in the flat space.</p> <p class="MsoNormal" style="text-align: justify;">Conclusion: Quantum mechanics on a circle exhibits many peculiar characteristics. Energy levels are discrete because of the geometry, in contrast to the configuration space of the real line. It presents a phase transition depending on the circle radius, also when embedded in a Kałuża&ndash;Klein model. This characteristic disappears when the radius becomes infinite, in the flat space.</p> Nicola Fabiano Copyright (c) 2026 Nikola Fabiano https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 11 25 10.5937/vojtehg74-58405 Contribution to the damage analysis of pipeline cracking under high pressure https://www.aseestant.ceon.rs/index.php/vtg/article/view/58675 <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Introduction/purpose: This study aims to contribute to the prediction of pipeline damage caused by cracking in hydrocarbon-transport pipelines, subjected to high internal pressures, in response to the growing demand in industrialised countries.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Methods: To achieve this objective and analyse crack propagation in terms of Stress Intensity Factor (SIF) evaluation, the Finite Element Method (FEM) was employed. The study considers the effects of the transported medium's internal pressure on the one hand, and external stresses caused by natural phenomena such as earthquakes, landslides, and others, on the other. These external stresses are represented by tensile and compressive forces. Particular attention was given to the propagation of three types of cracks: circumferential, longitudinal, and mixed-mode cracks.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Results: The affected tubular structure zone is highly susceptible to mode I cracking. In contrast to the two initial types of cracking defects, an oriented crack at an angle of &pi;/4 with respect to the pipeline's longitudinal axis develops nearly equally in modes I and II. Its growth kinetics are closely linked to its size, internal pressure, and the intensity of external forces.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Tensile forces promote the opening of circumferential cracks, the closure of longitudinal cracks, and mixed-mode (I and II) propagation of oriented cracks. Conversely, compressive forces favour the closure of circumferential and oriented cracks while encouraging the opening of longitudinal cracks.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Conclusion: The study reveals that, under identical loading conditions, longitudinally initiated cracks pose the greatest danger in terms of mode I crack growth. The risk of pipeline rupture is particularly high along the pipeline, and it increases significantly with higher internal pressure.</span></p> Fezazi Amina Ismahene Mechab Belaïd Salem Mokadem Serier Boualem Copyright (c) 2026 Fezazi Amina Ismahene https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 104 120 10.5937/vojtehg74-58675 Application of the FMECA method for identifying failures in wind turbine systems https://www.aseestant.ceon.rs/index.php/vtg/article/view/58801 <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">This paper presents the potential causes of component failures in wind turbine systems that affect their reliable and efficient operation. Component failures in wind turbines can lead to complete system failure, resulting in downtime, reduced reliability, and increased costs. To fully utilize wind energy, minimizing the risk of component failures is essential. By applying the FMECA method (Failure Mode Effects and Criticality Analysis &ndash; FMECA), critical components of wind turbine systems have been identified, providing the opportunity to prioritize problem-solving. The results emphasize the importance of maintenance and design optimization to reduce the risk of failures and maximize the utilization of wind energy.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Introduction/purpose: The reliability of wind turbine systems plays a crucial role in ensuring a stable and efficient electricity supply from renewable sources. The failure of any component can lead to system downtime, reduced reliability, and increased operational costs. In this context, it is essential to identify and analyze potential failures in order to improve overall system reliability. The aim of this paper is to analyze the reliability of a wind turbine system using the FMECA method. The focus is on identifying the most critical components and understanding the causes and consequences of their failures, thereby contributing to the improvement of system design, maintenance, and operation.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Methods: This paper applies the FMECA (Failure Modes, Effects, and Criticality Analysis) method, which enables a detailed assessment of potential system failures, their causes and effects, and the identification of the most critical system points based on quantitative parameters. The methodology includes the following steps:</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: Symbol; mso-fareast-font-family: Symbol; mso-bidi-font-family: Symbol; font-style: normal;"><span style="mso-list: Ignore;">&middot;<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Identification of key components of the wind turbine, including the rotor, gearbox, generator, control system, and other subsystems.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: Symbol; mso-fareast-font-family: Symbol; mso-bidi-font-family: Symbol; font-style: normal;"><span style="mso-list: Ignore;">&middot;<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Definition of possible failure modes for each component, with corresponding mechanisms that may lead to failure (e.g., wear, overheating, mechanical damage, etc.).</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: Symbol; mso-fareast-font-family: Symbol; mso-bidi-font-family: Symbol; font-style: normal;"><span style="mso-list: Ignore;">&middot;<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Evaluation of the consequences of failures, both on the specific component and on the overall operation of the wind turbine.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: Symbol; mso-fareast-font-family: Symbol; mso-bidi-font-family: Symbol; font-style: normal;"><span style="mso-list: Ignore;">&middot;<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Quantitative risk assessment through the assignment of values for:</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 114.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: 'Courier New'; mso-fareast-font-family: 'Courier New'; font-style: normal;"><span style="mso-list: Ignore;">o<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">the probability of potential failure occurrence (R<sub>1</sub>),</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 114.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: 'Courier New'; mso-fareast-font-family: 'Courier New'; font-style: normal;"><span style="mso-list: Ignore;">o<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">the severity of the potential failure (R<sub>2</sub>), and</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 114.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: 'Courier New'; mso-fareast-font-family: 'Courier New'; font-style: normal;"><span style="mso-list: Ignore;">o<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">the probability of detecting the failure and preventing its manifestation (R<sub>3</sub>).</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: Symbol; mso-fareast-font-family: Symbol; mso-bidi-font-family: Symbol; font-style: normal;"><span style="mso-list: Ignore;">&middot;<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Calculation of the criticality level (R) using the expression: </span><!-- [if gte msEquation 12]><m:oMath><span lang=sr style='font-family:"Cambria Math",serif'><m:r>R</m:r><m:r>=</m:r></span><m:sSub><m:sSubPr><span style='font-family:"Cambria Math",serif;mso-ascii-font-family:"Cambria Math"; mso-fareast-font-family:Batang;mso-hansi-font-family:"Cambria Math"'><m:ctrlPr></m:ctrlPr></span></m:sSubPr><m:e><span lang=sr style='font-family:"Cambria Math",serif'><m:r>R</m:r></span></m:e><m:sub><span lang=sr style='font-family:"Cambria Math",serif'><m:r>1</m:r></span></m:sub></m:sSub><span lang=sr style='font-family:"Cambria Math",serif'><m:r>∙</m:r></span><m:sSub><m:sSubPr><span style='font-family:"Cambria Math",serif;mso-ascii-font-family:"Cambria Math"; mso-fareast-font-family:Batang;mso-hansi-font-family:"Cambria Math"'><m:ctrlPr></m:ctrlPr></span></m:sSubPr><m:e><span lang=sr style='font-family:"Cambria Math",serif'><m:r>R</m:r></span></m:e><m:sub><span lang=sr style='font-family:"Cambria Math",serif'><m:r>2</m:r></span></m:sub></m:sSub><span lang=sr style='font-family:"Cambria Math",serif'><m:r>∙</m:r></span><m:sSub><m:sSubPr><span style='font-family:"Cambria Math",serif;mso-ascii-font-family:"Cambria Math"; mso-fareast-font-family:Batang;mso-hansi-font-family:"Cambria Math"'><m:ctrlPr></m:ctrlPr></span></m:sSubPr><m:e><span lang=sr style='font-family:"Cambria Math",serif'><m:r>R</m:r></span></m:e><m:sub><span lang=sr style='font-family:"Cambria Math",serif'><m:r>3</m:r></span></m:sub></m:sSub></m:oMath><![endif]--><!-- [if !msEquation]--> <!--[endif]--></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="font-family: Symbol; mso-fareast-font-family: Symbol; mso-bidi-font-family: Symbol; font-style: normal;"><span style="mso-list: Ignore;">&middot;<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Ranking of components based on R values to identify those that pose the greatest threat to system reliability and require prioritized monitoring or optimization.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Results: The results of the FMECA analysis indicate that the most critical components of the wind turbine system are:</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="mso-fareast-font-family: Arial;"><span style="mso-list: Ignore;">1.<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Gearbox &ndash; the highest criticality level (R value), as gearbox failure can lead to complete system shutdown and costly repairs.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin-left: 78.55pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="mso-fareast-font-family: Arial;"><span style="mso-list: Ignore;">2.<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Generator &ndash; high severity of failure and moderate likelihood of failure detection.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="margin: 0in 0in 0.0001pt 78.5pt; text-indent: -0.25in; text-align: justify;"><!-- [if !supportLists]--><span lang="sr" style="mso-fareast-font-family: Arial;"><span style="mso-list: Ignore;">3.<span style="font: 7.0pt 'Times New Roman';">&nbsp;&nbsp;&nbsp;&nbsp;&nbsp; </span></span></span><!--[endif]--><span lang="sr">Wind turbine control system &ndash; although failures are less frequent, the consequences can be severe due to the loss of control over the turbine.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Based on the analysis, components have been classified according to maintenance and monitoring priorities to enable timely detection of potential failures and prevent major breakdowns.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span lang="sr">Conclusion: The FMECA method has proven to be an effective tool for identifying and ranking potentially critical components of wind turbine systems. The results indicate that the gearbox, generator, and control system are the most sensitive points in the system. Their preventive maintenance, along with the implementation of condition monitoring systems and design improvements, can significantly enhance reliability and reduce operational costs. This analysis can serve as a foundation for improving maintenance strategies and increasing the operational efficiency of wind farms.</span></p> Branislava Radišić Copyright (c) 2026 Branislava Radišić https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 121 136 10.5937/vojtehg74-58801 Organic geochemical assessment of black shales: case study of Oued Soura, Tamtret region, Algeria https://www.aseestant.ceon.rs/index.php/vtg/article/view/59070 <p class="MsoNormal" style="text-align: justify;"><span style="font-family: 'Times New Roman','serif';">Introduction/purpose: Black shales are increasingly recognized as signif- icant unconventional hydrocarbon sources due to their organic richness and potential for oil and gas generation. However, their complex geo- chemical nature, especially in underexplored regions such as Tamtert in southwestern Algeria, poses challenges to accurate evaluation. This study aims to assess the hydrocarbon potential of black shales from the Djebel-Zereg area using advanced organic geochemical methods.</span></p> <p class="MsoNormal" style="text-align: justify;"><span style="font-family: 'Times New Roman','serif';">Methods: Five black shale samples were collected from Djebel-Zereg, Tamtert region. Total Organic Carbon (TOC) content was determined, and Rock-Eval 6 pyrolysis and elemental analysis were conducted. Pa- rameters measured included TOC, S1, S2, Tmax, Hydrogen Index (HI), Oxygen Index (OI), and vitrinite reflectance (Ro), providing data on or- ganic matter type, thermal maturity, and hydrocarbon generative capac- ity.</span></p> <p class="MsoNormal" style="text-align: justify;"><span style="font-family: 'Times New Roman','serif';">Results: TOC values ranged from 0.51 to 2 wt.% with an average of 1.33 wt.%, indicating acceptable to very good source rock quality. S2 values ranged from 0.45 to 4 mg HC/g rock, and the average Production Index (PI) was 2.23. HI values (51&ndash;233 mg HC/g TOC), along with OI and Tmax, indicated the presence of type II and III kerogen, suggesting potential for both oil and gas generation. Tmax values (435&ndash;465&deg;C, av- erage 447&deg;C) and vitrinite reflectance (0.68%&ndash;1.19%) confirmed thermal maturity. A positive correlation between TOC and S1 values supported the presence of indigenous hydrocarbons.</span></p> <p class="MsoNormal" style="text-align: justify;"><span style="font-family: 'Times New Roman','serif';">Conclusion: The integrated geochemical approach confirms that the Djebel-Zereg black shales are thermally mature, organic-rich rocks with promising oil shale potential. These findings support further explo- ration and development of unconventional hydrocarbon resources in the Tamtert region.</span></p> Abdelghani Kadou Boudjema Rebhi Copyright (c) 2026 Abdelghani Kadou https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 186 207 10.5937/vojtehg74-59070 A finite element-based optimization of composite wrap repair for welded pipelines with Surface Cracks: influence of geometry, adhesive properties, and internal pressure on mode I fracture behavior https://www.aseestant.ceon.rs/index.php/vtg/article/view/59078 <p class="S06cKeywordsatthebeginningofthearticle" style="text-align: justify;"><span lang="sr" style="color: black; letter-spacing: -.2pt; mso-bidi-font-style: normal;">Introduction/purpose: The structural integrity of pressurized pipelines is often threatened by surface cracks, especially in welded regions. This study evaluates the effectiveness of composite wrap reinforcement in repairing longitudinal semi-elliptical cracks in welded steel pipelines subjected to internal pressure. Although environmental effects such as temperature, moisture, and chemical exposure were not modeled, they are acknowledged as key factors influencing the long-term durability of composite repairs.</span></p> <p class="S06cKeywordsatthebeginningofthearticle" style="text-align: justify;"><span lang="sr" style="color: black; letter-spacing: -.2pt; mso-bidi-font-style: normal;">Methods: A three-dimensional finite element model was developed for a welded pipeline (outer diameter = 1016 mm, thickness = 12.8 mm) containing an external semi-elliptical crack (2c = 10.24 mm, a = 2.56 mm). The Virtual Crack Closure Technique (VCCT) was applied to compute Mode I Stress Intensity Factors (SIFs) under internal pressures of 2&ndash;12 MPa. A parametric study assessed the influence of patch length (100&ndash;400 mm), thickness (6&ndash;12 mm), and circumferential coverage angle (30&deg;&ndash;360&deg;), as well as adhesive shear modulus, thickness, and debonding effects.</span></p> <p class="S06cKeywordsatthebeginningofthearticle" style="text-align: justify;"><span lang="sr" style="color: black; letter-spacing: -.2pt; mso-bidi-font-style: normal;">Results: Increasing patch length, thickness, and coverage angle reduced SIFs, improving crack-tip stress attenuation. A higher adhesive shear modulus enhanced interfacial load transfer, while excessive adhesive thickness impaired efficiency. Localized adhesive debonding significantly increased SIFs under pressure, highlighting the sensitivity of repair performance to bonding quality.</span></p> <p class="S06cKeywordsatthebeginningofthearticle" style="text-align: justify;"><span lang="sr" style="color: black; letter-spacing: -.2pt; mso-bidi-font-style: normal;">Conclusions: This study provides design insights for optimizing composite reinforcement in welded pipeline repairs. Although a rectangular patch was analyzed, future work should investigate alternative geometries to mitigate edge stress concentrations and incorporate fatigue and environmental effects to better predict long-term service performance.</span></p> Hachemi Nedir Noureddine Mahmoudi Foudil Khelil Abed Bouadi Youcef Moulai Arbi Copyright (c) 2026 Hachemi Nedir, Noureddine mahmoudi, foudil khelil, Abed Bouadi, Youcef Moulai Arbi https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 155 185 10.5937/vojtehg74-59078 A new iteration scheme for approximating fixed points of some generalized nonexpansive mappings https://www.aseestant.ceon.rs/index.php/vtg/article/view/52039 <p style="text-align: justify;">Introduction/purpose: A new three-step iteration process, which converges faster than the Mann iteration and the S-iteration, is introduced, as well as some convergence results for approximation of fixed points of the Suzuki generalized nonexpansive mappings and nearly asymptotically nonexpansive mappings have been established.</p> <p style="text-align: justify;">Methods: The authors provide a specific three-step iterative method {xn} in a Banach space, defined as a sequence of convex combinations of the current iterate and its images under the mapping T, with control sequences {&alpha;n}, {&beta;n}, {&gamma;n} &sube; (0, 1). The results are proved in the setting of uniformly convex Banach spaces, where T is assumed to be either a Suzuki generalized nonexpansive mapping or a nearly asymptotically nonexpansive mapping. The authors obtain both weak and strong convergence theorems by using demiclosedness principles, Suzuki generalized nonexpansive mapping properties, and suitable lemmas on the behavior of the iterates. To compare the rates of convergence, they perform numerical experiments (usually implemented in MATLAB) where the proposed three-step iteration is run in parallel with the Thakur and S-iterations. The iterates are graphed to display the error convergence per iteration.</p> <p style="text-align: justify;">Results: The new iteration scheme converges faster than the S-iteration scheme if the mapping is a contraction. The new iteration scheme converges to a fixed point of a Suzuki generalized nonexpansive mapping under suitable conditions. The new iteration scheme converges to a fixed point of a nearly asymptotically nonexpansive mapping under suitable conditions.</p> <p style="text-align: justify;">Conclusions: The three-step iteration algorithm is proved, both theoretically and numerically, to converge faster than the Mann iteration and the S iteration (and sometimes faster than several other existing methods) for the considered types of mappings. The authors prove weak and strong convergence theorems for fixed points of the Suzuki generalized nonexpansive mappings and nearly asymptotically nonexpansive mappings in uniformly convex Banach spaces, thus generalizing, extending, and unifying several existing fixed-point approximation results in the literature.</p> Penumarthy Parvateesam Murthy Chandra Prakash Dhuri Copyright (c) 2025 Penumarthy Parvateesam MURTHY https://creativecommons.org/licenses/by/4.0 2026-01-20 2026-01-20 74 1 26 49 10.5937/vojtehg73-52039 Cryptography using Laplace transform for the Serbian language https://www.aseestant.ceon.rs/index.php/vtg/article/view/59148 <p class="MsoNormal" style="text-align: justify;">Introduction/purpose: In this paper authors develop a new mathematical method for cryptography. The procedure was performed for messages written in the Serbian language, which consists of 30 phonemes.</p> <p class="MsoNormal" style="text-align: justify;">Methods: The standard expansion of the inverse trigonometric function in a Taylor series was used. The Laplace transform was applied to encrypt the plaintext, while the corresponding inverse Laplace transform was used for decryption.</p> <p class="MsoNormal" style="text-align: justify;">Results: A new cryptographic algorithm has been written to encrypt and decrypt a text message written in Serbian letters.</p> <p class="MsoNormal" style="text-align: justify;">Conclusion: In the paper the authors presented a new algorithm in which the Laplace transform was used for the encryption and description of a message. The message is written in Serbian in Cyrillic letters.</p> Tatjana Mirković Nataša Ćirović Copyright (c) 2026 Tatjana Mirkovic https://creativecommons.org/licenses/by/4.0 2026-01-22 2026-01-22 74 1 1 10 10.5937/vojtehg74-59148 Battlesight zero in context of counter UAV engagement https://www.aseestant.ceon.rs/index.php/vtg/article/view/59713 <p><!-- [if gte mso 9]><xml> <o:OfficeDocumentSettings> <o:RelyOnVML/> <o:AllowPNG/> </o:OfficeDocumentSettings> </xml><![endif]--><!-- [if gte mso 9]><xml> <w:WordDocument> <w:View>Normal</w:View> <w:Zoom>0</w:Zoom> <w:TrackMoves/> <w:TrackFormatting/> <w:HyphenationZone>21</w:HyphenationZone> <w:PunctuationKerning/> <w:ValidateAgainstSchemas/> <w:SaveIfXMLInvalid>false</w:SaveIfXMLInvalid> <w:IgnoreMixedContent>false</w:IgnoreMixedContent> <w:AlwaysShowPlaceholderText>false</w:AlwaysShowPlaceholderText> <w:DoNotPromoteQF/> <w:LidThemeOther>EN-US</w:LidThemeOther> <w:LidThemeAsian>X-NONE</w:LidThemeAsian> 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Name="List Table 7 Colorful Accent 5"/> <w:LsdException Locked="false" Priority="46" Name="List Table 1 Light Accent 6"/> <w:LsdException Locked="false" Priority="47" Name="List Table 2 Accent 6"/> <w:LsdException Locked="false" Priority="48" Name="List Table 3 Accent 6"/> <w:LsdException Locked="false" Priority="49" Name="List Table 4 Accent 6"/> <w:LsdException Locked="false" Priority="50" Name="List Table 5 Dark Accent 6"/> <w:LsdException Locked="false" Priority="51" Name="List Table 6 Colorful Accent 6"/> <w:LsdException Locked="false" Priority="52" Name="List Table 7 Colorful Accent 6"/> <w:LsdException Locked="false" SemiHidden="true" UnhideWhenUsed="true" Name="Mention"/> <w:LsdException Locked="false" SemiHidden="true" UnhideWhenUsed="true" Name="Smart Hyperlink"/> <w:LsdException Locked="false" SemiHidden="true" UnhideWhenUsed="true" Name="Hashtag"/> <w:LsdException Locked="false" SemiHidden="true" UnhideWhenUsed="true" Name="Unresolved Mention"/> <w:LsdException Locked="false" SemiHidden="true" UnhideWhenUsed="true" Name="Smart Link"/> </w:LatentStyles> </xml><![endif]--><!-- [if gte mso 10]> <style> /* Style Definitions */ table.MsoNormalTable {mso-style-name:"Normální tabulka"; mso-tstyle-rowband-size:0; mso-tstyle-colband-size:0; mso-style-noshow:yes; mso-style-priority:99; mso-style-parent:""; mso-padding-alt:0cm 5.4pt 0cm 5.4pt; mso-para-margin:0cm; mso-pagination:widow-orphan; font-size:10.0pt; font-family:"Times New Roman",serif; mso-ansi-language:EN-US; mso-fareast-language:EN-US;} </style> <![endif]--></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span style="font-family: 'Times New Roman'; font-size: medium;">Introduction/purpose: This paper explores the optimal zeroing distance for an assault rifle on the modern battlefield. Traditionally, armies have used sight settings that align the projectile&rsquo;s trajectory with the line of sight at distances of 25 m and 300 m. This configuration is well suited for assault rifles chambered in 7 mm to 8 mm calibers when fired from the prone position at an approaching figure target. However, with the increasing use of smaller-caliber ammunition (5 mm to 6 mm) and evolving battlefield threats, including drones, it is necessary to reassess this traditional approach. This study investigates the optimal first zeroing distance when engaging both drone-type targets and standard NATO Type E figure targets. All tests and configurations were conducted using the BREN 2 assault rifle used by the Czech Army. </span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span style="font-family: 'Times New Roman'; font-size: medium;">Methods: This study uses probability-of-hit simulation methods. The parameters of the BREN 2 weapon under investigation were experimentally verified.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span style="font-family: 'Times New Roman'; font-size: medium;">Results: The probability of hitting a point target depends significantly on the setting of the sight zeroing distance. The greater the deviation of the projectile trajectory from the line of sight, the lower the probability of hitting the target without distance adjustment.</span></p> <p class="S06bAbstracttextatthebeginningofthearticle" style="text-align: justify;"><span style="font-family: 'Times New Roman'; font-size: medium;">Conclusion: The findings suggest that for engaging small, irregular targets such as UAVs, zeroing distances between 50 m and 100 m are more effective, without compromising combat effectiveness against standard figure targets.</span></p> Ivan Pemčák Copyright (c) 2026 Ivan Pemčák https://creativecommons.org/licenses/by/4.0 2026-01-22 2026-01-22 74 1 137 154 10.5937/vojtehg74-59713 Call for papers and instructions for authors for the issue 1-2026 https://www.aseestant.ceon.rs/index.php/vtg/article/view/65828 Vladan Anicijevic Copyright (c) 2026 Vladan Anicijevic https://creativecommons.org/licenses/by/4.0 2026-03-18 2026-03-18 74 1 244 254 10.5937/vojtehg74-65828 The list of the reviewers of the Military Technical Courier in 20245 https://www.aseestant.ceon.rs/index.php/vtg/article/view/65830 Vladan Anicijevic Copyright (c) 2026 Vladan Anicijevic https://creativecommons.org/licenses/by/4.0 2026-03-18 2026-03-18 74 1 255 255 10.5937/vojtehg74-65830 Publication ethics statement for the year 2026 https://www.aseestant.ceon.rs/index.php/vtg/article/view/65831 Vladan Anicijevic Copyright (c) 2026 Vladan Anicijevic https://creativecommons.org/licenses/by/4.0 2026-03-18 2026-03-18 74 1 256 268 10.5937/vojtehg74-65831 Back impressum for the issue 1-2026 https://www.aseestant.ceon.rs/index.php/vtg/article/view/65832 Vladan Anicijevic Copyright (c) 2026 Vladan Anicijevic https://creativecommons.org/licenses/by/4.0 2026-03-18 2026-03-18 74 1 10.5937/vojtehg74-65832