Defence Technology(防务技术)最新文献

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Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA 使用非多项式高阶 IGA 的蜂窝-FGS 壳体在动态载荷作用下的动态响应
IF 5
Defence Technology(防务技术) Pub Date : 2024-07-01 DOI: 10.1016/j.dt.2023.12.002
Pham Binh Le, Trung-Thanh Tran
{"title":"Dynamic response of honeycomb-FGS shells subjected to the dynamic loading using non-polynomial higher-order IGA","authors":"Pham Binh Le,&nbsp;Trung-Thanh Tran","doi":"10.1016/j.dt.2023.12.002","DOIUrl":"10.1016/j.dt.2023.12.002","url":null,"abstract":"<div><p>The main goal of this study is to use higher-order isogeometric analysis (IGA) to study the dynamic response of sandwich shells with an auxetic honeycomb core and two different functionally graded materials (FGM) skin layers (namely honeycomb-FGS shells) subjected to dynamic loading. Touratier's non-polynomial higher-order shear deformation theory (HSDT) is used due to its simplicity and performance. The governing equation is derived from Hamilton's principle. After verifying the present approach, the effect of input parameters on the dynamic response of honeycomb-FGS shells is carried out in detail.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"37 ","pages":"Pages 149-161"},"PeriodicalIF":5.0,"publicationDate":"2024-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914723003252/pdfft?md5=a245042fde2d01f63a460f642e161677&pid=1-s2.0-S2214914723003252-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"138690484","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Multidisciplinary design optimization of a dual-spin guided vehicle 双自旋制导飞行器多学科设计优化
IF 5
Defence Technology(防务技术) Pub Date : 2024-07-01 DOI: 10.1016/j.dt.2023.11.025
Jalal Karimi, Mohammad Reza Rajabi, Seyed Hossein Sadati, Seyed Mahid Hosseini
{"title":"Multidisciplinary design optimization of a dual-spin guided vehicle","authors":"Jalal Karimi,&nbsp;Mohammad Reza Rajabi,&nbsp;Seyed Hossein Sadati,&nbsp;Seyed Mahid Hosseini","doi":"10.1016/j.dt.2023.11.025","DOIUrl":"10.1016/j.dt.2023.11.025","url":null,"abstract":"<div><p>In this research, a Multidisciplinary Design Optimization approach is proposed for the dual-spin guided flying projectile design considering external and internal parts of the body as design variables. In this way, a parametric formulation is developed. All related disciplines, including structure, aerodynamics, guidance, and control are considered. Minimum total mass, maximum aerodynamic control effectiveness, minimum miss distance, maximum yield stress in all subsystems, controllability and gyroscopic stability constraints are some of objectives/constraints taken into account. The problem is formulated in All-At-Ones Multidisciplinary Design Optimization approach structure and solved by Simulated Annealing and minimax algorithms. The optimal configurations are evaluated in various aspects. The resulted optimal configurations have met all design objectives and constraints.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"37 ","pages":"Pages 133-148"},"PeriodicalIF":5.0,"publicationDate":"2024-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914723003227/pdfft?md5=e3b6e0f031bd71907010c2e96e008733&pid=1-s2.0-S2214914723003227-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"138520191","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Color-polarization synergistic target detection method considering shadow interference 考虑阴影干扰的彩色偏振协同目标探测方法
IF 5
Defence Technology(防务技术) Pub Date : 2024-07-01 DOI: 10.1016/j.dt.2024.01.007
Bin Feng , Jinpei Xiao , Junchao Zhang , Lin Li , Yunlong Wu , Qing Ye
{"title":"Color-polarization synergistic target detection method considering shadow interference","authors":"Bin Feng ,&nbsp;Jinpei Xiao ,&nbsp;Junchao Zhang ,&nbsp;Lin Li ,&nbsp;Yunlong Wu ,&nbsp;Qing Ye","doi":"10.1016/j.dt.2024.01.007","DOIUrl":"10.1016/j.dt.2024.01.007","url":null,"abstract":"<div><p>Aiming at the problem of shadow interference in UAV's ground reconnaissance, a color and polarization synergistic target detection method is proposed for <em>anti</em>-shadow interference, based on the influence of two physical characteristics (wavelength and polarization) under different illuminations. A valid fusion strategy is proposed via integrating two separate detection results on color and polarization images. Moreover, a local enhancement and recognition module (LER) is introduced to boost the performance. Based on our built dataset, experimental results show that our method achieves <em>m</em><sub>AP</sub> of 87.76%, and 12.37% higher than that of color image and 14.68% higher than that of polarization image.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"37 ","pages":"Pages 50-61"},"PeriodicalIF":5.0,"publicationDate":"2024-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914724000229/pdfft?md5=6ca92757207cd8d3a89d985b21addb96&pid=1-s2.0-S2214914724000229-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140150798","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Explosion damage effects of aviation kerosene storage tank under strong ignition 强点火下航空煤油储罐的爆炸破坏效应
IF 5
Defence Technology(防务技术) Pub Date : 2024-07-01 DOI: 10.1016/j.dt.2023.12.009
Shixiang Song, Cheng Wang, Boyang Qiao, Gongtian Gu
{"title":"Explosion damage effects of aviation kerosene storage tank under strong ignition","authors":"Shixiang Song,&nbsp;Cheng Wang,&nbsp;Boyang Qiao,&nbsp;Gongtian Gu","doi":"10.1016/j.dt.2023.12.009","DOIUrl":"10.1016/j.dt.2023.12.009","url":null,"abstract":"<div><p>In order to study the blast damage effects of aviation kerosene storage tanks, the out-field explosion experiments of 8 m³ fixed-roof tanks were carried out. The fragments, shock wave and fireball thermal radiation of the tank in the presence of bottom oil, half oil and full oil, as well as empty tank, were investigated under internal explosion by various TNT charge contents (1.8 kg, 3.5 kg and 6.2 kg). The results showed that the tank roof was the only fragment produced, and the damage forms could be divided into three types. The increase of TNT charge content and oil volume enlarged the deformation of the tank, while the hole ratio presented a trend of increase first and then decrease. The <em>H</em><sub>r, max</sub> and <em>V</em><sub>max</sub> values positively increased as increasing the TNT charge content and oil volume (from empty to half oil), but decreased in full oil. The <em>P</em><sub>max</sub> values had a progressive increase with the increment of TNT charge content, but not the case with the increase in oil volumes. The development of fireball was divided into three stages: tank roof ‘towed’ flame, jet flow flame tumbling and rising, and jet flow flame extinguishing. The <em>D</em><sub>max</sub> and <em>H</em><sub>f, max</sub> values both increased as increasing TNT charge content and oil volumes. The oscillation phenomenon of fireball temperature was observed in the cooling process. The average temperature of fireball surface was positively correlated with TNT charge content, and negatively correlated with oil volumes.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"37 ","pages":"Pages 27-38"},"PeriodicalIF":5.0,"publicationDate":"2024-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S221491472300332X/pdfft?md5=03bc41f374349043823e9ba87a7ea08e&pid=1-s2.0-S221491472300332X-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"138993849","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A brand new green coating technology for realizing the regulation of spherical propellant energy release process 实现球形推进剂能量释放过程调控的全新绿色涂层技术
IF 5.1
Defence Technology(防务技术) Pub Date : 2024-06-01 DOI: 10.1016/j.dt.2024.02.008
Wenhao Fan , Yajun Ding , Zhongliang Xiao
{"title":"A brand new green coating technology for realizing the regulation of spherical propellant energy release process","authors":"Wenhao Fan ,&nbsp;Yajun Ding ,&nbsp;Zhongliang Xiao","doi":"10.1016/j.dt.2024.02.008","DOIUrl":"10.1016/j.dt.2024.02.008","url":null,"abstract":"<div><p>To achieve the controllable release of energy of nitrocellulose-based propellants, this paper combines the cellulose-based nanocomposites aqueous coating (Surelease®-NC) with fluidized bed coating equipment to successfully prepare the coated spherical propellant for the first time. The effects of fluidized bed coating temperature, air velocity, flow speed and atomization pressure on the adhesion rate, coating integrity and coating uniformity of the coated spherical propellant were investigated, and the preparation of coated spherical propellant with homogeneous size and structural integrity was achieved for the first time. The microscopic morphology, chemical structure, water vapor adsorption behavior, combustion performance, and ageing resistance property of the coated spherical propellant were systematically investigated by, Fourier transforms infrared spectroscopy (FTIR), Micro confocal raman spectrometer, field scanning electron microscopy (SEM), dynamic vapor adsorption techniques, and closed bomb test, confirming the surface core-shell structure and the tightly bonded interfacial structure of coated spherical propellant. Meanwhile, the coated spherical propellant has good hygroscopic, excellent progressive burning and long storage stability.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 78-94"},"PeriodicalIF":5.1,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914724000369/pdfft?md5=2c86cb5dd92add02475d35ba8ddbc4d5&pid=1-s2.0-S2214914724000369-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140003932","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Applicability limits of the DAX test in plastic bonded explosives DAX 试验在塑料粘结炸药中的适用极限
IF 5.1
Defence Technology(防务技术) Pub Date : 2024-06-01 DOI: 10.1016/j.dt.2023.09.009
Martin Künzel , Jindrich Kucera , Jiri Pachman
{"title":"Applicability limits of the DAX test in plastic bonded explosives","authors":"Martin Künzel ,&nbsp;Jindrich Kucera ,&nbsp;Jiri Pachman","doi":"10.1016/j.dt.2023.09.009","DOIUrl":"10.1016/j.dt.2023.09.009","url":null,"abstract":"<div><p>The Disc Acceleration eXperiment (DAX) is one of the most recent experimental methods of performance characterization of new energetic materials. A cylindrical explosive charge accelerates a thin metallic disc and its velocity is measured continuously using photonic Doppler velocimetry. The detonation velocity is measured simultaneously. The DAX test can be used to obtain the Chapman-Jouguet (CJ) detonation pressure and to describe detonation products expansion using reduced amount of explosive. A series of DAX tests was performed at various charge diameters and disc thicknesses with Semtex 1 A plastic bonded explosive and sensitized nitromethane. The DAX-like evaluation was also applied to previously measured data of Semtex 1A and A-IX-1 explosives. The optimum disc thickness is determined by the disc to explosive mass ratio of 0.01–0.08. The repeatability of the Semtex 1 A detonation pressure results is about four times lower compared to the pressed and liquid explosives.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 64-70"},"PeriodicalIF":5.1,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914723002532/pdfft?md5=9b6fd7cb6cf13cee8d77cc6b929b702a&pid=1-s2.0-S2214914723002532-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"135434394","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Revisiting the theoretical prediction of the explosive performance found by the Trauzl test 对Trauzl试验爆炸性能理论预测的修正
IF 5.1
Defence Technology(防务技术) Pub Date : 2024-06-01 DOI: 10.1016/j.dt.2023.08.013
Ivana Dobrilovic, Mario Dobrilovic, Muhamed Suceska
{"title":"Revisiting the theoretical prediction of the explosive performance found by the Trauzl test","authors":"Ivana Dobrilovic,&nbsp;Mario Dobrilovic,&nbsp;Muhamed Suceska","doi":"10.1016/j.dt.2023.08.013","DOIUrl":"10.1016/j.dt.2023.08.013","url":null,"abstract":"<div><p>The Trauzl lead block test allows the determination of the approximate performance of explosives in blasting applications by measuring the volume increase (expansion) that is produced by the detonation of an explosive charge in the cavity of a lead block. In this paper, we reconsider the possibility of interpreting the Trauzl test results in terms of detonation parameters or quantities. The detonation parameters used in the analysis are calculated using the thermochemical code EXPLO5, while the hydrocode AUTODYN is used to simulate the effect of explosive charge density and reaction rate on the results of the Trauzl test. The increase in the volume of the lead block cavity was found to correlate best with the product of the detonation heat and the root of the volume of detonation products. Hydrocode simulation showed that the density of explosive charge and the rate of explosive decomposition affect the dynamics of the interaction of the detonation product and the lead block, and consequently the lead block cavity volume increase.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 163-174"},"PeriodicalIF":5.1,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914723002283/pdfft?md5=98a60b62e8c84308d0177f9e767fb92f&pid=1-s2.0-S2214914723002283-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"46730447","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Energy and blast performance of beryllium in a model thermobaric composition in comparison with aluminum and magnesium 铍与铝和镁在模型热压成分中的能量和爆炸性能比较
IF 5.1
Defence Technology(防务技术) Pub Date : 2024-06-01 DOI: 10.1016/j.dt.2024.02.011
Thomas M. Klapötke , Stanisław Cudziło , Waldemar A. Trzciński , Józef Paszula
{"title":"Energy and blast performance of beryllium in a model thermobaric composition in comparison with aluminum and magnesium","authors":"Thomas M. Klapötke ,&nbsp;Stanisław Cudziło ,&nbsp;Waldemar A. Trzciński ,&nbsp;Józef Paszula","doi":"10.1016/j.dt.2024.02.011","DOIUrl":"10.1016/j.dt.2024.02.011","url":null,"abstract":"<div><p>A direct comparison is made between the effectiveness of Al, Mg, and Be powders as additional fuels in model thermobaric compositions containing 20% fuel, 20% ammonium perchlorate, and 60% RDX (1,3,5-Trinitro-1,3,5-triazacyclohexane) passivated with wax. Experimentally determined calorimetric measurements of the heat of detonation, along with the overpressure histories in an explosion chamber filled with nitrogen, were used to determine the quasi-static pressure (QSP) under anaerobic conditions. Overpressure measurements were also performed in a semi-closed bunker, and all blast wave parameters generated after the detonation of 500 g charges of the tested explosives were determined. Detonation calorimetry results, QSP values, and blast wave parameters (pressure amplitude, specific and total impulses) clearly indicate that Be is much more effective as an additional fuel than either Al or Mg in both anaerobic post-detonation reactions as well as the subsequent aerobic combustion. The heat of detonation of the RDXwax/AP/Be explosive mixture is over 40% and 50% higher than that of the mixture containing aluminum and magnesium instead of beryllium, respectively. Moreover, the TNT equivalent of the Be-containing composition due to the overpressure in the nitrogen-filled explosion chamber is 1.66, while the equivalent calculated using an air shock wave-specific impulse at a distance of 2.5 m is equal to 1.69. The high values of these parameters confirm the high reactivity of beryllium in both the anaerobic and aerobic stages of the thermobaric explosion.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 13-19"},"PeriodicalIF":5.1,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914724000540/pdfft?md5=9a44514ad283766c2690b0a9cd113e8c&pid=1-s2.0-S2214914724000540-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"140401173","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Development of vehicle- recognition method on water surfaces using LiDAR data: SPD2 (spherically stratified point projection with diameter and distance) 利用激光雷达数据开发水面车辆识别方法:SPD2(带直径和距离的球面分层点投影)
IF 5.1
Defence Technology(防务技术) Pub Date : 2024-06-01 DOI: 10.1016/j.dt.2023.09.013
Eon-ho Lee , Hyeon Jun Jeon , Jinwoo Choi , Hyun-Taek Choi , Sejin Lee
{"title":"Development of vehicle- recognition method on water surfaces using LiDAR data: SPD2 (spherically stratified point projection with diameter and distance)","authors":"Eon-ho Lee ,&nbsp;Hyeon Jun Jeon ,&nbsp;Jinwoo Choi ,&nbsp;Hyun-Taek Choi ,&nbsp;Sejin Lee","doi":"10.1016/j.dt.2023.09.013","DOIUrl":"10.1016/j.dt.2023.09.013","url":null,"abstract":"<div><p>Swarm robot systems are an important application of autonomous unmanned surface vehicles on water surfaces. For monitoring natural environments and conducting security activities within a certain range using a surface vehicle, the swarm robot system is more efficient than the operation of a single object as the former can reduce cost and save time. It is necessary to detect adjacent surface obstacles robustly to operate a cluster of unmanned surface vehicles. For this purpose, a LiDAR (light detection and ranging) sensor is used as it can simultaneously obtain 3D information for all directions, relatively robustly and accurately, irrespective of the surrounding environmental conditions. Although the GPS (global-positioning-system) error range exists, obtaining measurements of the surface-vessel position can still ensure stability during platoon maneuvering. In this study, a three-layer convolutional neural network is applied to classify types of surface vehicles. The aim of this approach is to redefine the sparse 3D point cloud data as 2D image data with a connotative meaning and subsequently utilize this transformed data for object classification purposes. Hence, we have proposed a descriptor that converts the 3D point cloud data into 2D image data. To use this descriptor effectively, it is necessary to perform a clustering operation that separates the point clouds for each object. We developed voxel-based clustering for the point cloud clustering. Furthermore, using the descriptor, 3D point cloud data can be converted into a 2D feature image, and the converted 2D image is provided as an input value to the network. We intend to verify the validity of the proposed 3D point cloud feature descriptor by using experimental data in the simulator. Furthermore, we explore the feasibility of real-time object classification within this framework.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 95-104"},"PeriodicalIF":5.1,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S221491472300257X/pdfft?md5=65ce532c6fc955391046fadd1a2856d1&pid=1-s2.0-S221491472300257X-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"134961949","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Experimental crushing behavior and energy absorption of angular gradient honeycomb structures under quasi-static and dynamic compression 角梯度蜂窝结构在准静态和动态压缩下的挤压行为和能量吸收实验
IF 5.1
Defence Technology(防务技术) Pub Date : 2024-06-01 DOI: 10.1016/j.dt.2024.02.002
Jiachen Li , Yuchen Wei , Hao Wu , Xingyu Shen , Mengqi Yuan
{"title":"Experimental crushing behavior and energy absorption of angular gradient honeycomb structures under quasi-static and dynamic compression","authors":"Jiachen Li ,&nbsp;Yuchen Wei ,&nbsp;Hao Wu ,&nbsp;Xingyu Shen ,&nbsp;Mengqi Yuan","doi":"10.1016/j.dt.2024.02.002","DOIUrl":"10.1016/j.dt.2024.02.002","url":null,"abstract":"<div><p>The high variability of shock in terrorist attacks poses a threat to people's lives and properties, necessitating the development of more effective protective structures. This study focuses on the angle gradient and proposes four different configurations of concave hexagonal honeycomb structures. The structures' macroscopic deformation behavior, stress-strain relationship, and energy dissipation characteristics are evaluated through quasi-static compression and Hopkinson pressure bar impact experiments. The study reveals that, under varying strain rates, the structures deform starting from the weak layer and exhibit significant interlayer separation. Additionally, interlayer shear slip becomes more pronounced with increasing strain rate. In terms of quasi-static compression, symmetric gradient structures demonstrate superior energy absorption, particularly the symmetric negative gradient structure (SNG-SMS) with a specific energy absorption of 13.77 J/cm³. For dynamic impact, unidirectional gradient structures exhibit exceptional energy absorption, particularly the unidirectional positive gradient honeycomb structure (UPG-SML) with outstanding mechanical properties. The angle gradient design plays a crucial role in determining the structure's stability and deformation mode during impact. Fewer interlayer separations result in a more pronounced negative Poisson's ratio effect and enhance the structure's energy absorption capacity. These findings provide a foundation for the rational design and selection of seismic protection structures in different strain rate impact environments.</p></div>","PeriodicalId":58209,"journal":{"name":"Defence Technology(防务技术)","volume":"36 ","pages":"Pages 47-63"},"PeriodicalIF":5.1,"publicationDate":"2024-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://www.sciencedirect.com/science/article/pii/S2214914724000205/pdfft?md5=2f5cc2de920b80313d953d5463271728&pid=1-s2.0-S2214914724000205-main.pdf","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"139927456","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
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