Relevant bibliographies by topics / Honeycomb structures

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Honeycomb structures'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 August 2024

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Journal articles on the topic "Honeycomb structures"

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Alkhader, Maen, Bassam Abu-Nabah, Mostafa Elyoussef, and T. A. Venkatesh. "Design of honeycomb structures with tunable acoustic properties." MRS Advances 4, no. 44-45 (2019): 2409–18. http://dx.doi.org/10.1557/adv.2019.355.

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ABSTRACTHoneycomb structures, owing to their microstructural periodicity, exhibit unique and complex acoustic properties. Tuning their acoustic properties typically involves either changing their topology or porosity. The former route can lead to topologies that may not be readily amenable for large-scale production, while the latter could negatively affect the honeycombs’ weight. An ideal approach for tailoring the acoustic behavior of honeycombs should neither affect their porosity nor should they require customized and expensive fabrication methods. In this work, a novel honeycomb design th
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Li, Jiaxing, Weizhou Zhong, Jian Li, Yuan Liu, and Zexiong Zhang. "Influence of Cell Pore Configuration on Dynamic Mechanical Properties of Honeycomb Structures." Journal of Physics: Conference Series 2660, no. 1 (2023): 012006. http://dx.doi.org/10.1088/1742-6596/2660/1/012006.

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Abstract With the rapid development of advanced manufacturing technologies such as additive manufacturing, which provides an effective means for processing and preparing a variety of structures with more complex geometrical configurations, the design and study of honeycomb structures have played an important role in promoting the design and study of honeycomb structures. At present, the study of such structures is mainly limited to hexagonal honeycombs, and relatively few studies have been conducted on other cell geometries. In this study, by using the finite element method, we have simulated
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Wang, Yan, P. Xue, and J. P. Wang. "Comparing Study of Energy-Absorbing Behavior for Honeycomb Structures." Key Engineering Materials 462-463 (January 2011): 13–17. http://dx.doi.org/10.4028/www.scientific.net/kem.462-463.13.

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Honeycomb materials，as a type of ultra-light multifunctional material，have been examined extensively in recent years and have been applied in many fields. This study investigated the energy absorption capacity and their mechanisms of honeycomb structures with five different cell geometry (square，triangular，circular, hexagonal，kagome). It has been shown that the honeycomb structure with kagome cells is the best choice under the targets of the energy absorption capacity, peak force and plateau stress, when relative density and cell wall thickness of the five kinds of honeycombs are the same. Bes
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Khan, Tayyab, Alia Ruzanna Aziz, Muhammad S. Irfan, Wesley J. Cantwell, and Rehan Umer. "Energy absorption in carbon fiber honeycomb structures manufactured using a liquid thermoplastic resin." Journal of Composite Materials 56, no. 9 (2022): 1335–48. http://dx.doi.org/10.1177/00219983221073985.

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In this study, carbon fiber/thermoplastic (Elium®) honeycombs were manufactured using the resin infusion process in a customized metallic mold. Honeycomb cores, based on different carbon fiber layers, were manufactured to achieve four different fiber weight fraction composites. Two different types of specimens, based on a single honeycomb cell and five honeycomb cells, were prepared and subjected to compression loading. The results of these tests were compared with data from similar honeycomb structures based on carbon fiber–reinforced epoxy composite. It has been shown that the compressive st
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Wang, Zhiping, Gang Chen, Xiaofei Cao, Wei Chen, Chun Bao Li, and Xiaobin Li. "Study on the Effect of Nodal Configuration on the Mechanical Properties of Hexa-Ligamentous Chiral Honeycombs." Journal of Marine Science and Engineering 11, no. 9 (2023): 1692. http://dx.doi.org/10.3390/jmse11091692.

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To investigate the effect of nodal configuration on the mechanical properties of hexachiral honeycombs, three specimens, namely, a standard honeycomb, a thickened-node honeycomb, and a filled-node honeycomb, were prepared using 3D-printing technology. Several quasi-static compression tests were performed, which revealed that nodal reinforcement can inhibit nodal aberrations during ligament winding, thus facilitating the “rotational” mechanism and improving the negative Poisson’s ratio properties of the honeycomb. Experiments performed using the finite element method showed that nodal reinforce
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Kondratiev, Andrii, Oksana Prontsevych, and Tetyana Nabokina. "Analysis of the Bearing Capacity of Adhesive Joint of Honeycomb Cores of Sandwich Structures with the Continuous Adhesive Layer." Key Engineering Materials 864 (September 2020): 228–40. http://dx.doi.org/10.4028/www.scientific.net/kem.864.228.

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Adhesive sandwich structures with the honeycomb core of the metallic foil, polymeric papers and composites are widely and effectively used in the units of aerospace engineering and in the other industries owing to a number of undeniable advantages, including high specific strength and stiffness. In the process of designing and manufacturing of abovementioned structures, it is necessary to ensure high strength and reliability of the adhesive joint of the bearing skins and honeycomb core at a small area of their contact. The decisive factors influencing the bearing capacity of such joint are the
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Shirbhate, P. A., and M. D. Goel. "Effect of Reinforcement in Energy Absorption Characteristics of Honeycomb Structures Under Blast Loading." Proceedings of the 12th Structural Engineering Convention, SEC 2022: Themes 1-2 1, no. 1 (2022): 1231–35. http://dx.doi.org/10.38208/acp.v1.645.

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During recent decades demand for cellular structures has increased due to raised concern for protection of important buildings and components from blast loads. These types of cellular materials possess important features that includes less weight, higher energy absorption capabilities, higher strength to weight ratio in comparison with monolithic counterpart. Cellular material includes honeycomb, corrugated, web type structure, open and closed cell metal foam etc. However, in the present investigation, honeycomb sandwich panel are rein forced and are analysed for blast response mitigation. Fur
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Oettinger, Marcel, Tim Kluge, and Joerg Seume. "Influence of honeycomb structures on labyrinth seal aerodynamics." Journal of the Global Power and Propulsion Society 6 (October 19, 2022): 290–303. http://dx.doi.org/10.33737/jgpps/152697.

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Shroud cavities in aero engines are typically formed by a labyrinth seal between the rotating turbine shroud and the stationary casing wall. To mitigate rub-in and reduce weight, the casing often features honeycomb structures above the rotor seal fins. In this paper, the aerodynamic performance of such honeycomb structures is experimentally investigated using a rotating test rig featuring both smooth and honeycomb-tapered casing walls. Measurements show that the discharge coefficient decreases for the honeycomb configuration while losses and subsequent windage heating of the flow increase. A v
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Li, Xiangcheng, Kang Li, Yuliang Lin, Rong Chen, and Fangyun Lu. "Inserting Stress Analysis of Combined Hexagonal Aluminum Honeycombs." Shock and Vibration 2016 (2016): 1–10. http://dx.doi.org/10.1155/2016/3240651.

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Two kinds of hexagonal aluminum honeycombs are tested to study their out-of-plane crushing behavior. In the tests, honeycomb samples, including single hexagonal aluminum honeycomb (SHAH) samples and two stack-up combined hexagonal aluminum honeycombs (CHAH) samples, are compressed at a fixed quasistatic loading rate. The results show that the inserting process of CHAH can erase the initial peak stress that occurred in SHAH. Meanwhile, energy-absorbing property of combined honeycomb samples is more beneficial than the one of single honeycomb sample with the same thickness if the two types of ho
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Wang, A. J., and D. L. McDowell. "In-Plane Stiffness and Yield Strength of Periodic Metal Honeycombs." Journal of Engineering Materials and Technology 126, no. 2 (2004): 137–56. http://dx.doi.org/10.1115/1.1646165.

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In-plane mechanical properties of periodic honeycomb structures with seven different cell types are investigated in this paper. Emphasis is placed on honeycombs with relative density between 0.1 and 0.3, such that initial yield is associated with short column compression or bending, occurring prior to elastic buckling. Effective elastic stiffness and initial yield strength of these metal honeycombs under in-plane compression, shear, and diagonal compression (for cell structures that manifest in-plane anisotropy) are reported as functions of relative density. Comparison among different honeycom
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Dissertations / Theses on the topic "Honeycomb structures"

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Favre, Benoit. "Crushing properties of hexagonal adhesively bonded honeycombs loaded in their tubular direction." Thesis, Atlanta, Ga. : Georgia Institute of Technology, 2007. http://hdl.handle.net/1853/22620.

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Thesis (M. S.)--Civil and Environmental Engineering, Georgia Institute of Technology, 2007.<br>Committee Chair: Mulalo Doyoyo; Committee Co-Chair: Reginald Desroches; Committee Member: Laurence J. Jacobs.
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Petras, Achilles. "Design of sandwich structures." Thesis, University of Cambridge, 1999. https://www.repository.cam.ac.uk/handle/1810/236995.

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Failure modes for sandwich beams of GFRP laminate skins and Nomex honeycomb core are investigated. Theoretical models using honeycomb mechanics and classical beam theory are described. A failure mode map for loading under 3-point bending, is constructed, showing the dependence of failure mode and load on the ratio of skin thickness to span length and honeycomb relative density. Beam specimens are tested in 3-point bending. The effect of honeycomb direction is also examined. The experimental data agree satisfactorily with the theoretical predictions. The results reveal the important role of cor
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Shafizadeh, Jahan Emir. "Processing and characterization of honeycomb composite systems /." Thesis, Connect to this title online; UW restricted, 1999. http://hdl.handle.net/1773/9830.

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Liang, T. "Electrohydrodynamic forming of honeycomb-like polymeric structures." Thesis, University College London (University of London), 2015. http://discovery.ucl.ac.uk/1464210/.

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In this dissertation, polyethylene oxide (PEO) and ethyl cellulose (EC) have been chosen as model polymers to investigate different aspects of electrohydrodynamic processing and forming. In the first part of the work, electrospraying of PEO was attempted choosing a wide range of single solvents and mixed solvents. The selection of solvents affects the solubility and spinnability of PEO and the morphology of electrospun fibres. In the second part of the research the creation of 3D nanofibrous structures using electrospinning of PEO was investigated. The results demonstrate how the process is in
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Copenhaver, David C. "Thermal characterization of honeycomb core sandwich structures." Thesis, This resource online, 1996. http://scholar.lib.vt.edu/theses/available/etd-11182008-063547/.

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Yu, Zhaohui Crocker Malcolm J. "Static, dynamic and acoustical properties of sandwich composite materials." Auburn, Ala., 2007. http://repo.lib.auburn.edu/2006%20Fall/Dissertations/YU_ZHAOHUI_54.pdf.

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Martin, Cary Joseph. "Prepreg effects on honeycomb composite manufacturing /." Thesis, Connect to this title online; UW restricted, 1998. http://hdl.handle.net/1773/9861.

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Church, Benjamin Cortright. "High conductivity alloys for extruded metallic honeycomb." Thesis, Georgia Institute of Technology, 2002. http://hdl.handle.net/1853/21283.

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Seay, Wesley Daniel. "Capillary rheometric evaluation of honeycomb extrusion pastes." Thesis, Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/18951.

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Wong, Kok Hou Centre for Advanced Macromolecular Design Faculty of Engineering UNSW. "Honeycomb structured porous film from amphiphilic block copolymers for biomedical applications." Awarded by:University of New South Wales. Centre for Advanced Macromolecular Design, 2008. http://handle.unsw.edu.au/1959.4/41493.

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In recent times, it was divulged that highly ordered honeycomb structured porous films from a variety of polymers could be fabricated by breath figures (water droplets) templating technique. In contrast to existing macroporous fabrication techniques, this technique is simple, more versatile and very cost effective. Amphiphilic block copolymers composed of a hydrophobic and a hydrophilic block were employed in this research to examine the process of porous film formation and the outcome of films generated using breath figure technique. A customized film casting system, established according to
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Books on the topic "Honeycomb structures"

1

C, Thompson Randolph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Titanium honeycomb panel testing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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C, Thompson Randolph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Titanium honeycomb panel testing. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

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3

Daigaku, Keiō Gijuku, HTA kenkyūkai, HTA Association, and Shinkenchikusha, eds. Hanikamu chūbu ākitekuchā tekunorojī bukku. Shinkenchikusha, 2009.

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Weichuan, Lin, Mbanefo Uy, and Langley Research Center, eds. Facesheet wrinkling in sandwich structures. National Aeronautics and Space Administration, Langley Research Center, 1999.

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Walker, Sandra P. Evaluation of composite honeycomb sandwich panels under compressive loads at elevated temperatures. National Aeronautics and Space Administration, Langley Research Center, 1998.

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Bitzer, Tom. Honeycomb technology: Materials, design, manufacturing, applications and testing. Chapman & Hall, 1997.

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M, Jensen, Grant L, and Langley Research Center, eds. High temperature be panel development. National Aeronautics and Space Administration, Langley Research Center, 1989.

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A, Ivanov A. Novoe pokolenie sotovykh zapolniteleĭ dli︠a︡ aviat︠s︡ionno-kosmicheskoĭ tekhniki. Ėnergoatomizdat, 2000.

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Endogur, A. I. Sotovye konstrukt͡s︡ii: Vybor parametrov i proektirovanie. "Mashinostroenie", 1986.

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Tao, Zhang. Study of impact damage of Nomex honeycomb sandwich plates. School of Aeronautics, Harbin Institute of Technology, 1989.

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Book chapters on the topic "Honeycomb structures"

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Melcher, Jörg. "Piezoceramic Honeycomb Actuators." In Adaptive, tolerant and efficient composite structures. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-29190-6_8.

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John, Małgorzata, Antoni John, and Łukasz Kanicki. "Numerical Testing of Honeycomb Structures." In Applied Condition Monitoring. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-62042-8_38.

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Ikeda, Kiyohiro, and Kazuo Murota. "Flower Patterns on Honeycomb Structures." In Imperfect Bifurcation in Structures and Materials. Springer New York, 2010. http://dx.doi.org/10.1007/978-1-4419-7296-5_16.

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Ikeda, Kiyohiro, and Kazuo Murota. "Flower Patterns on Honeycomb Structures." In Imperfect Bifurcation in Structures and Materials. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-21473-9_17.

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Zeng, Qiang, Shenqiang Feng, and Zhengkai Zhang. "Optimization of Impact Resistant Structures with Negative Poisson’s Ratio Based on Response Surface Methodology." In Lecture Notes in Civil Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-4355-1_34.

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AbstractIn order to enhance the blast resistance capabilities of critical structural elements in buildings, a blast-resistant honeycomb sandwich protective structure based on a negative Poisson’s ratio structure was proposed and designed. The failure mechanisms of the protective structure under distributed impulse loads were investigated. The structural parameters of the protective structure were optimized using the response surface methodology, and simulation analysis was conducted using the finite element method. The results demonstrate that the optimized negative Poisson’s ratio honeycomb sandwich protective structure exhibits excellent blast resistance performance.
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Wang, M., X. Qiu, and X. Zhang. "Mechanical Properties of Super Honeycomb Structures." In Computational Mechanics. Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-75999-7_75.

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Chandrashekhar, A., Himam Saheb Shaik, S. Ranjan Mishra, Tushar Srivastava, and M. L. Pavan Kishore. "Static Structural Analysis of Hybrid Honeycomb Structures Using FEA." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-7557-0_32.

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Guo, N., and M. K. Lim. "Lamb Waves Propagation in Aluminum Honeycomb Structures." In Review of Progress in Quantitative Nondestructive Evaluation. Springer US, 1996. http://dx.doi.org/10.1007/978-1-4613-0383-1_41.

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Apollonov, Victor V. "Large POEs Based on Multilayer Honeycomb Structures." In Springer Series in Optical Sciences. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-10753-0_11.

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Elmer, Thomas H. "Selective Leaching of Extruded Cordierite Honeycomb Structures." In Ceramic Engineering and Science Proceedings. John Wiley & Sons, Inc., 2008. http://dx.doi.org/10.1002/9780470320310.ch4.

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Conference papers on the topic "Honeycomb structures"

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Watkins, Ryan T., John A. Shaw, Nicolas Triantafyllidis, and David Grummon. "Design Study of Shape Memory Alloy Honeycombs for Energy Absorption." In ASME 2011 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. ASMEDC, 2011. http://dx.doi.org/10.1115/smasis2011-5091.

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Shape memory alloys (SMA), which exhibit the shape memory effect and superelasticity, utilize a reversible solid-solid state phase transformation to recover large strains. Likewise, honeycomb structures under in-plane loading take advantage of deformation kinematics to amplify the structure’s macroscopic strain. The combination of a sparse honeycomb structure made of an SMA material can recover larger deformations than would be possible with either conventional metal honeycombs or monolithic SMAs. NiTi honeycombs and corrugations of about 5% relative density with robust properties were demonst
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Brown, C., E. Verghese, D. Sporer, and R. Sellors. "PM2000 Honeycomb Structures." In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/98-gt-565.

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The use of oxide dispersion strengthened (ODS) superalloys for excellent high temperature oxidation resistance has been well established. This is achieved by the formation of a dense, slowly growing and tightly adherent alumina scale on Fe-Cr-Al and Ni-Cr-Al ODS alloys. The addition of oxide dispersion strengthening confers a structural capability for operation temperatures of up to 1350°C. Traditionally these materials have been used in relatively thick sections where the core “reservoir” of aluminium is adequate to provide a continuous replenishment of the protective oxide coating. This pape
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Ju, Jaehyung, Joshua D. Summers, John Ziegert, and George Fadel. "Compliant Hexagonal Meso-Structures Having Both High Shear Strength and High Shear Strain." In ASME 2010 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/detc2010-28672.

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Motivated by the authors’ previous study on flexible honeycomb design with negative Poisson’s ratio (NPR) often called ‘auxetic’ [1], more geometric options of hexagonal honeycomb meso-structures are explored with various ratios of the vertical cell length, h to the inclined length, l. While designing an effective shear modulus, e.g., G12* of 10MPa, of hexagonal honeycombs, we are searching honeycomb geometries. Using an aluminum alloy (7075-T6) as the constituent material, the in-plane linear elastic honeycomb model is employed to get effective shear moduli, effective shear yield strengths an
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Nast, Eckart, and Eckart Nast. "On honeycomb-type core moduli." In 38th Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1178.

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Zhan, Chi, Mingzhe Li, Robert McCoy, Linda Zhao, and Weiyi Lu. "3D-Printed Hierarchical Re-Entrant Honeycomb With Improved Structural Stability Under Quasi-Static Compressive Loading." In ASME 2021 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/imece2021-68961.

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Abstract Re-entrant honeycombs with negative Poisson’s ratio have shown great potential as lightweight energy absorbers for various applications. However, due to its bending-dominated behavior, the structural stability and energy absorption capacity of reentrant honeycombs are yet to be further improved. It has been demonstrated that hierarchical structures exhibit a combination of lightweight and superior mechanical properties. We hypothesize that by introducing the triangular hierarchical substructures into the conventional cell walls, the bending-dominated behavior of re-entrant honeycombs
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Rahman, Kazi Moshiur, Todd Letcher, and Zhong Hu. "Effects of Defects on the Performance of Hierarchical Honeycomb Metamaterials Realized Through Additive Manufacturing." In ASME 2016 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/imece2016-66940.

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Cellular metamaterials are of immense interest for many current engineering applications. Tailoring the structural organization of cellular structures leads to new metamaterials with superior properties leading to low weight and very strong/stiff materials. Incorporation of hierarchy to regular cellular structures enhances the properties and introduces novel tailorable metamaterials. For many complex cellular metamaterials, the only realistic manufacturing process is additive manufacturing (AM). The use of AM to manufacture large structures may lead to several types of defects during the manuf
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Karagiozova, Dora, and Marcilio Alves. "On the Energy Absorption of Combined Foam-Honeycomb Layered Structures." In ASME 2016 35th International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/omae2016-54471.

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Analytical and numerical analyses are carried in order to reveal the importance of the topology of the cellular materials for their dynamic compaction. The aim is to distinguish between the deformation mechanisms and energy absorption of materials, which exhibit structural softening, such as out-of-plane loaded honeycomb, and structural hardening (foam). It is shown that the dynamic compaction of honeycombs does not obey the law of shock wave propagation and a new phenomenological model of the velocity attenuation in out-of plane loaded honeycomb is proposed. Comparisons with some currently av
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Oettinger, Marcel, Tim Kluge, and Joerg R. Seume. "INFLUENCE OF HONEYCOMB STRUCTURES ON LABYRINTH SEAL AERODYNAMICS." In GPPS Xi'an21. GPPS, 2022. http://dx.doi.org/10.33737/gpps21-tc-339.

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Shroud cavities in aero engines are typically formed by a labyrinth seal between the rotating turbine blade and the stationary casing wall. To mitigate rub-in and reduce weight, the casing often features honeycomb structures above the rotor seal fins. In this paper, the aerodynamic performance of such honeycomb structures is experimentally investigated using a rotating test rig featuring both smooth and honeycomb-tapered casing walls. Measurements show that the discharge coefficient decreases for the honeycomb configuration while losses and subsequent windage heating of the flow increase. A va
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Heo, Hyeonu, Jaehyung Ju, Doo-Man Kim, and Chang-Soo Jeon. "Passive Morphing Airfoil With Honeycombs." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-64350.

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A passive morphing may improve the aerodynamic characteristics through structural shape change by aerodynamic loads during the flight, resulting in improving fuel efficiency. The passive morphing structure should have a capability to be highly deformed while maintaining a sufficient stiffness in bending. Honeycombs may be good for controlling both stiffness and flexibility. This paper investigates a honeycomb airfoil’s static deformations through the fluid-structure interaction using computational fluid dynamics and structural finite element analysis. The structural performance will be investi
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Hassan, Mohd R., F. Scarpa, N. A. Mohammed, and Y. Ancrenaz. "Conventional and Auxetic SMA Cellular Structures." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-81075.

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This work illustrates the manufacturing and tensile testing of a novel concept of honeycomb structures with hexagonal and auxetic (negative Poisson’s ratio) topology, made of shape memory alloy (SMA) core material. The honeycombs are manufactured using Nitinol ribbons having 6.40 mm of width and 0.2 mm of thickness. The ribbons were inserted in a special dye using cyanoacrilate to bond the longitudinal strips of the unit cells. The ribbons were subjected to tensile test at room temperature (martensite finish) and austenite finish temperature. Tensile tests at room temperature were performed on
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Reports on the topic "Honeycomb structures"

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STRUCTURAL MORPHOLOGY AND DYNAMIC CHARACTERISTICS ANALYSIS OF DRUM-SHAPED HONEYCOMB-TYPE III CABLE DOME WITH QUAD-STRUT LAYOUT. The Hong Kong Institute of Steel Construction, 2024. http://dx.doi.org/10.18057/ijasc.2024.20.1.9.

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