Relevant bibliographies by topics / Composite bonded joints

Contents

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

Academic literature on the topic 'Composite bonded joints'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "Composite bonded joints"

1

Motlhakudi, I., and A. Jonker. "Fatigue Characterisation of Adhesives Used in Fibre-Reinforced Composites." R&D Journal 39 (2023): 53–79. http://dx.doi.org/10.17159/2309-8988/2023/v39a6.

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A review of past investigations into the fatigue behaviour of structural adhesives and bonded joints in fibre-reinforced polymer composites is given. An overview of the structural adhesives used in general bonded joint applications is first provided, followed by an experimental fatigue testing of these bonded components. The aspects that influence fatigue strength and fatigue life for adhesively bonded joints in fibre-reinforced polymer composites are then discussed in terms of the adhesive composition, geometry configuration, surface condition and preparation, and loading conditions. The aspe
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Ghoneam, S. M., A. A. Hamada, and M. I. El-Elamy. "Experimental and Analytical Investigations of the Dynamic Analysis of Adhesively Bonded Joints for Composite Structures." Solid State Phenomena 147-149 (January 2009): 663–75. http://dx.doi.org/10.4028/www.scientific.net/ssp.147-149.663.

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Adhesively bonded joints are used extensively in various industries. Some imperfections like holes, thermal residual stresses occurring in the bolted, welded, riveted, and soldered joints don't take place in adhesively bonded joints. Hence, the main advantages of bonded joint are lightness, sealing, corrosion resistance, heat and sound isolation, damping, and quickly mounting facility which have been highly proved. This paper introduces an attempt to study the dynamic analysis of adhesively bonded joint for composite structures to investigate mainly the influences of lamina code number, bonded
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Hart-Smith, L. J. "Bonded-bolted composite joints." Journal of Aircraft 22, no. 11 (1985): 993–1000. http://dx.doi.org/10.2514/3.45237.

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Kulkarni, Santosh, Devendra Singh, Laeth Hussain, et al. "Finite element analysis of bonded, riveted and hybrid joints in glass fibre epoxy composite laminates for aircraft structure." E3S Web of Conferences 563 (2024): 02006. http://dx.doi.org/10.1051/e3sconf/202456302006.

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Because of their superior fatigue resistance and high strength-to-weight ratio, composite materials are essential to the construction of modern airplanes. The joints that interconnect the various parts of these structures play a critical role in their integrity and functionality. In aerospace applications, bonded, riveted, and hybrid joints are among the many types of joints that are frequently used. A thorough finite element analysis (FEA) of hybrid, bonded, and riveted joints in glass fiber epoxy composite laminates for airplane structures is presented in this work. The literature review add
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Liu, Longquan. "A study of the damage tolerance of composite-metal hybrid joints reinforced by multiple and penetrative thin pins." Composites and Advanced Materials 31 (January 2022): 263498332211055. http://dx.doi.org/10.1177/26349833221105523.

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The application of adhesive bonding technology in aircraft structures can reduce the total wight greatly, but the bonded joints are very sensitive to the possible manufacturing defects and damages during service operations, which makes them difficult to meet the damage tolerance requirements of the current transport airplane structures. In this study, the damage tolerance of composite-metal hybrid joints reinforced by multiple and penetrative thin pins was studied. The damage tolerance performance of the composite-metal joint is supposed to be enhanced by multiple through-the-thickness penetra
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Lokhande, Rupesh, Abhijeet Deshpande, and Ashok Mache. "Taguchi Analysis of Bonded Single-Lap Joint in Hemp Fiber Composite." International Journal of Engineering Technology and Sciences 3, no. 1 (2016): 27–33. http://dx.doi.org/10.15282/ijets.5.2016.1.4.1043.

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The adhesively bonded joints in composite structures are widely used in aerospace and automobile fields. Hemp epoxy composites are better alternative due to its lower specific gravity and higher toughness. . The joining process is inevitable in the application of such composites. The mechanical behaviour of such joints depends on the strength of the composite, adhesive strength and adhesion phenomenon between substrate and adhesive. The influence of overlap length, adhesive layer thickness and cure temperature on the performance of adhesive joints investigated experimentally. The influence of
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ATMAKURI, Ayyappa, Arvydas PALEVICIUS, Madhusudan SIDDABATHULA, and Giedrius JANUŠAS. "Failure Studies on Adhesive Bonded and Bolted Joints of Natural Fiber Composites." Mechanics 27, no. 5 (2021): 392–99. http://dx.doi.org/10.5755/j02.mech.28108.

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Composites with natural fibers as reinforcements are playing a vital role in recent developments. The present work deals with the fabrication of okra and empty fruit bunch banana fiber polyester matrix composites with varying reinforcement content (5%, 10%, and 15%). Composites were fabricated by using the hand layup technique. After the fabrication process, composites were then adhesively bonded and also joined with bolts. The main objective of this work is to analyse the failure studies on adhesive bonded and bolted joints of okra and empty fruit bunch banana composite specimens. The specime
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P, Prasad, Sreenivasa Murthy B. P, and Thimmegowda M. B. "Bonded Composite Laminates (E-Glass to Graphite) Failure Analysis Subjected to Axial Tension." International Journal for Research in Applied Science and Engineering Technology 12, no. 12 (2024): 1146–55. https://doi.org/10.22214/ijraset.2024.65986.

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Abstract: Researchers studied influence of various parameters on the failure behaviour on metal and composite joints. The one of the challenge in analysis of bonded joints of dissimilar materials of the stress and strain fields at the adhesive layer and adherents. The adhesive bonded joints are most used in present technology in aerospace engineering, mechanical engineering, automotive sectors and civil engineering. This work is based on numerical tools of engineering structures adhesion problems. The proposed numerical tools are implemented Finite Element Method (FEM). A numerical methods bas
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Nagayya, M. K. Venkatesh, N. Nithesh Bhaskar, and B. K. Venkatesha. "Strength analysis of carbon fiber reinforced polymer and titanium alloy for axisymmetric lap joint." Journal of Mines, Metals and Fuels 69, no. 12A (2022): 137. http://dx.doi.org/10.18311/jmmf/2021/30142.

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Many industries such as oil, gas, aerospace, and automotive, use axisymmetric adhesively bonded single lap joints. Different materials are frequently mated using axisymmetric lap joints. When composite adherents delaminate, the stress circulation inside the adhesive layer significantly influenced. As a result, the importance of considering adhesive layer stresses in the presence of considerable delamination is investigated in this paper. To understand stress analysis and examine adhesive bond strength at static loading conditions, the model created using finite element analysis with cohesive z
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Kim, Won Seock, and Jung Ju Lee. "Interfacial Fracture Analysis of Adhesive-Bonded Joints." Advanced Materials Research 33-37 (March 2008): 327–32. http://dx.doi.org/10.4028/www.scientific.net/amr.33-37.327.

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The failure in an adhesive-bonded structure starts at the interface, and the interfacial fracture is of interest whenever adhesion between different materials is concerned. One of primary factors limiting the application of adhesive-bonded joints to structural design is the lack of a good evaluation tool for adhesion strength to predict the load-bearing capacity of boned joints. The adhesion strength of composite/steel bonding has been evaluated using interfacial fracture mechanics characterization. The energy release rate of a composite/steel interfacial crack was compared with the fracture t
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Dissertations / Theses on the topic "Composite bonded joints"

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Ficarra, Christina Helene. "ANALYSIS OF ADHESIVE BONDED FIBER-REINFORCED COMPOSITE JOINTS." NCSU, 2001. http://www.lib.ncsu.edu/theses/available/etd-20010626-155040.

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<p>The work presented in this thesis involved the analysis of adhesive bonded joints for composite bridge decks and was divided into three phases. The first phase involved a parametric study on a single lap joint using ANSYS finite element analysis software. The purpose of the parametric study was to alter the geometry and material properties of the joint and study their effects on the stress distribution in both the adherends and adhesive. The four different cases studied included adding a taper to the adherends, different edge shapes on the adhesive layer, a material stiffness imbalance and
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Shāhid, Muḥammad. "Adhesion characterisation of bonded steel/composite cleavage joints." Thesis, University of Glasgow, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.402470.

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Osiyemi, Stephen Olusegun. "The fatigue performance of adhesively bonded fibre-composite joints." Thesis, Imperial College London, 1992. http://hdl.handle.net/10044/1/7971.

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Brett, Michael Alexander de Oliveira. "Prediction of the performance of adhesively-bonded composite joints." Thesis, Imperial College London, 2012. http://hdl.handle.net/10044/1/9545.

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The use of adhesively-bonded joints instead of the traditional types of joining can give reduced weight and increased stiffness in a structure. However, most industries have concerns about the use of adhesive joints in anything other than secondary structures, due to uncertainties over the long-term service life. This thesis discusses the prediction of the lifetime of adhesively-bonded composite structures. A fracture mechanics approach was used to characterise the fracture behaviour of an epoxy film adhesive, Cytec FM-300M, mainly using composite substrates prepared using wet peel ply, removi
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Pillai, Govind Ramakrishna Lankarani Hamid M. "Response of adhesively bonded composite joints to low velocity impact." Diss., A link to full text of this thesis in SOAR, 2006. http://soar.wichita.edu/dspace/handle/10057/676.

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Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Mechanical Engineering.<br>"December 2006." Title from PDF title page (viewed on Nov. 4, 2007). Thesis adviser: Hamid M. Lankarani. Includes bibliographic references (leaves 64-67).
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Mosher, Bryan C. "Failure Prediction of Adhesively Bonded Hardboard Doorskin Joints." Thesis, Virginia Tech, 2005. http://hdl.handle.net/10919/42867.

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Wood and wood based composites such as hardboard have become very common materials for use in non-structural applications, which include pre-finished paneling, siding, exterior trim, furniture, and door skins. This thesis describes the results of a study of the failure of hardboard door skins. Forces applied during manufacture load the door skins in bending, and in some cases cause a split at the edge of the hardboard. A finite element model as well as a closed form solution based on mechanics of materials were developed to analyze the stresses and deformations of the door skin/stile assemb
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Pohlit, David Joseph. "Dynamic Mixed-Mode Fracture of Bonded Composite Joints for Automotive Crashworthiness." Thesis, Virginia Tech, 2007. http://hdl.handle.net/10919/33837.

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An experimental evaluation of the mixed-mode fracture behavior of bonded composite joints is presented. Commonly used experimental techniques for characterizing the mode I, mixed-mode I/II, mode II, and mode III fracture behavior have been employed for the purpose of developing a fracture envelope to be utilized in the automotive design process. These techniques make use of such test geometries as the double cantilever beam (DCB), asymmetric double cantilever beam (ADCB), single-leg bend (SLB), end-loaded split (ELS), and split cantilever beam (SCB) specimens. Symmetric versions of the DCB,
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Wang, Xiao. "Stress-Function Variational Methods for Stress Analysis of Composite Laminates and Adhesively Bonded Composite Joints." Thesis, North Dakota State University, 2015. https://hdl.handle.net/10365/27639.

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Adhesively bonded composite joints (ABCJs) have been broadly used to connect multimaterials and show their structural and economic advantages compared to traditional bonding methods. However, robust methods are still desired for efficient and accurate lay-wise stress analysis of ABCJs involving multiple boundaries and layers. The purpose of this work was to extend the stress-function variational method for free-edge stress analysis of composite laminates with a finite length. At each interface of the laminate, two unknown Lehknitskii?s stress potential functions were introduced to interp
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Radice, Joshua J. "The analysis and design of adhesively bonded composite structures." Access to citation, abstract and download form provided by ProQuest Information and Learning Company; downloadable PDF file 1.10Mb , 279 p, 2005. http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&res_dat=xri:pqdiss&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&rft_dat=xri:pqdiss:3181889.

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Tiu, W. P. "Fatigue strength prediction of adhesively bonded unidirectional carbon fibre reinforced composite joints." Thesis, City University London, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.378857.

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Books on the topic "Composite bonded joints"

1

Cheng, Jinquan. Smart adhesively bonded composite joints: Analysis and design. Nova Science, 2009.

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Chamis, C. C. Simplified procedures for designing adhesively bonded composite joints. National Aeronautics and Space Administration, 1989.

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3

S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. National Aeronautics and Space Administration, Langley Research Center, 1985.

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S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. National Aeronautics and Space Administration, Langley Research Center, 1985.

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S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. National Aeronautics and Space Administration, Langley Research Center, 1985.

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S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. National Aeronautics and Space Administration, Langley Research Center, 1985.

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K, Kochhar N., and Langley Research Center, eds. Criterion for mixed mode fracture in composite bonded joints. National Aeronautics and Space Administration, Langley Research Center, 1986.

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Ali, Rezaizadeh Mohammad, Ramamurthy G, and Langley Research Center, eds. Interaction of mixed mode loading on cyclic debonding in adhesively bonded composite joints. National Aeronautics and Space Administration, Langley Research Center, 1985.

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9

S, Johnson W., Everett R. A, and Langley Research Center, eds. Effect of adherend thickness and mixed mode loading on debond growth in adhesively bonded composite joints. National Aeronautics and Space Administration, Langley Research Center, 1986.

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Hoeven, W. van der. Static and fatigue strength of an adhesive bonded CFRP butt-strap joint, the effects of stacking sequence and temperature. National Aerospace Laboratory, 1988.

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Book chapters on the topic "Composite bonded joints"

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Marr, G. R., R. P. Barrowcliffe, and A. R. Curtis. "The Non-destructive Evaluation of Composite Bonded Joints." In Composite Structures 3. Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-4952-2_35.

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Kim, Hyonny. "Analytical Modeling for Composite Structures." In Strength Prediction of Adhesively-Bonded Joints. CRC Press, 2017. http://dx.doi.org/10.1201/9781315370835-3.

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Hart-Smith, L. J. "Adhesively Bonded Joints for Fibrous Composite Structures." In Recent Advances in Structural Joints and Repairs for Composite Materials. Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0329-1_6.

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Dhilipkumar, Thulasidhas, and Murugan Rajesh. "Adhesively Bonded Composite Joints in Aerospace Application." In Repair of Advanced Composites for Aerospace Applications. CRC Press, 2022. http://dx.doi.org/10.1201/9781003200994-7.

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Tong, L., J. K. Spelt, and G. Fernlund. "Strength Determination of Adhesive Bonded Joints." In Recent Advances in Structural Joints and Repairs for Composite Materials. Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0329-1_2.

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Vinson, Jack R. "Laminated Shells and Adhesive Bonded Joints." In The Behavior of Shells Composed of Isotropic and Composite Materials. Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-015-8141-7_9.

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Mao, Jianghui, Sayed A. Nassar, and Xianjie Yang. "A Model for Fracture Characterization of Adhesively-Bonded Joints." In Composite Materials and Joining Technologies for Composites, Volume 7. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-4553-1_9.

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Curtis, A. R., and P. D. Ainsworth. "The Mechanical Testing and Computer Modelling of Composite Bonded Joints." In Composite Structures 3. Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-4952-2_39.

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Tserpes, Konstantinos, Elli Moutsompegka, Mareike Schlag, et al. "Characterization of Pre-bond Contamination and Aging Effects for CFRP Bonded Joints Using Reference Laboratory Methods, Mechanical Tests, and Numerical Simulation." In Adhesive Bonding of Aircraft Composite Structures. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-319-92810-4_2.

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AbstractIn this chapter, the pre-bond contamination and ageing effects on carbon fiber reinforced plastic (CFRP) adherends and CFRP bonded joints are characterized by means of reference laboratory non-destructive testing (NDT) methods, mechanical tests, and numerical simulation. Contaminations from two fields of application are considered, namely in aircraft manufacturing (i.e. production) and for in-service bonded repair. The production-related scenarios comprise release agent, moisture, and fingerprint, while the repair-related scenarios comprise fingerprint, thermal degradation, de-icing fl
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Gupta, Mohit, Matteo Mazzotti, Daniel Cantrell, et al. "Guided Wave-Based Assessment of Bonded Composite Joints." In Lecture Notes in Civil Engineering. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-07322-9_25.

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Conference papers on the topic "Composite bonded joints"

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Gollins, Kenneth, Jack Chiu, Céline Baudrand, and Feridun Delale. "Characterization of Adhesively Bonded Composite Joints Under High Strain Rate Loading." In ASME 2017 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/imece2017-71711.

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With the advantage of having a high strength to weight ratio, composite materials are frequently being implemented as alternatives to steel and aluminum in military vehicles. To perform satisfactorily, joined composite laminates on a vehicle must be able to absorb a significant amount of energy under high strain rate loading events such as ballistic impact. In this paper the dynamic behavior and failure modes of adhesively bonded S2-glass/epoxy laminate joints are investigated. For this experiment, two structural adhesives are selected for comparison: a brittle methacrylate and a more complian
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Anwar, Iqbal, and Golam Newaz. "Computational Approach for Adhesively Bonded Composite Joints." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2476.

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Abstract A computational intensive study was performed to assess an efficient way to model adhesively bonded glass fiber reinforced composite joints in automotive applications. Three different finite element modeling techniques had been implemented. First, adhesive was represented by 1D-spring elements. Spring stiffness was calculated from adhesive property. This model is inadequate to assess stresses developed in the adhesive layer directly. So adhesive was modeled with 2D elements for better assessment of state of stress in the adhesive and the substrate. Both the model provide limit load, b
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Action, Jason, and Stephen P. Engelstad. "Crack Arrestment of Bonded Composite Joints." In 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-1876.

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Tsai, Hsi, James Alper, and David Barrett. "Failure analysis of composite bonded joints." In 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-1428.

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Dvorak, George J., Jian Zhang, and Olcay Canyurt. "Adhesive Joints for Composite Sandwich Structures." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-2034.

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Abstract A new approach is explored for joining of thick, woven E-glass/vinyl ester composite laminated plates to steel or composite plates, with applications in naval ship structures. Adhesive is applied along through-the-thickness contoured interfaces, employing tongue-and-groove geometry. Both experimental and finite element modeling results are presented. They show that adhesively bonded tongue-and-groove joints between steel and composite plates loaded in monotonically increasing longitudinal tension, are stronger than conventional strap joints even in relatively thin plates. In particula
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Otheguy, M., A. G. Gibson, and A. M. Robinson. "Towards Recyclable Composite Craft: Fusion Bonded Thermoplastic Composite T-Joints." In Marine & Offshore Composites. RINA, 2010. http://dx.doi.org/10.3940/rina.moc10cd.2010.04.

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Flansburg, Barrett, Stephen Engelstad, and Jim Lua. "Robust Design of Composite Bonded Pi Joints." In 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2447.

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Oterkus, Erkan, Atila Barut, Erdogan Madenci, and Damodar Ambur. "Analysis of Bolted-Bonded Composite Lap Joints." In 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-2187.

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Cox, S., S. Danley, J. Wright, A. Nettles, W. Guin, and K. Segal. "Composite Repair Process for Adhesively Bonded Joints." In CAMX 2019. NA SAMPE, 2019. http://dx.doi.org/10.33599/nasampe/c.19.0696.

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Yarrington, Phil, James Zhang, Craig Collier, and Brett Bednarcyk. "Failure Analysis of Adhesively Bonded Composite Joints." In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-2376.

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Reports on the topic "Composite bonded joints"

1

Tsai, Hsi C., James Alper, and David Barrett. Failure Analysis of Composite Bonded Joints. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada375743.

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Madenci, Erdogan. An Inverse Approach for Capturing the Interaction of Macro- and Micro-Scales in Characterizing Bonded Composite Joints. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada387637.

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