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Littérature scientifique sur le sujet « Bonded structures »

Auteur : Grafiati
Publié le 4 juin 2021
Mis à jour le 2 février 2022

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Articles de revues sur le sujet "Bonded structures"

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Takagi, Nozomi, et Shigeru Nagase. « Tin Analogues of Alkynes. Multiply Bonded Structures vs Singly Bonded Structures ». Organometallics 26, no 3 (janvier 2007) : 469–71. http://dx.doi.org/10.1021/om060993v.

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Bishop, Roger, Donald C. Craig, Vi T. Nguyen et Marcia L. Scudder. « Dialcohol Hydrogen Bonded Ladder Structures ». Molecular Crystals and Liquid Crystals 390, no 1 (1 janvier 2003) : 19–25. http://dx.doi.org/10.1080/10587250216163.

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WEAIRE, D., C. O’CARROLL et M. AL-HOURANI. « EQUILIBRATION OF TETRAHEDRALLY BONDED STRUCTURES ». Modern Physics Letters B 01, no 01n02 (mai 1987) : 39–47. http://dx.doi.org/10.1142/s0217984987000065.

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Tetrahedrally bonded structures, of the kind used in the study of amorphous silicon, are often relaxed to minimise energy within a simple potential scheme such as that of Keating. We discuss how this may be executed in a simple but highly efficient manner, as is desirable whenever the structure is modified many times in a Monte Carlo calculation.
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Luckyram, Jeenarainsingh, et Alan E. Vardy. « Shear displacement in bonded structures ». Journal of Constructional Steel Research 16, no 1 (janvier 1990) : 71–84. http://dx.doi.org/10.1016/0143-974x(90)90005-2.

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Oumeraci, Hocine, Tijl Staal, Saskia Pfoertner, Matthias Kudella, Stefan Schimmels et Henk Jan Verhagen. « HYDRAULIC PERFORMANCE OF ELASTOMERIC BONDED PERMEABLE REVETMENTS AND SUBSOIL RESPONSE TO WAVE LOADS ». Coastal Engineering Proceedings 1, no 32 (21 janvier 2011) : 22. http://dx.doi.org/10.9753/icce.v32.structures.22.

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Elastomeric bonded permeable revetments, also called PBA (Polyurethane bonded aggregate) revetments, are highly porous structures made of mineral aggregates (e.g. crushed stones) which are durably and elastically bonded by polyurethane (PU). Despite their numerous advantages as compared to conventional revetments and the large experience available from more than 25 pilot projects, physically-based design formulae to predict their hydraulic performance, wave loading and response are still lacking. Therefore, the present study aims at improving the understanding of the processes involved in the interaction between wave, revetment and foundation, based on large-scale model tests performed in the Coastal Research Centre (FZK), Hannover/Germany, and to provide prediction formulae/diagrams. This paper is focused on the prediction of the hydraulic performance (wave reflection, wave run-up and run-down) and the response of the sand core (pore pressure and effective stress) beneath the revetment for a wide range of wave conditions, including the analysis of an observed failure due to transient soil liquefaction.
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Liebisch, Sven, Juan Carlos Alcérreca Huerta, Andreas Kortenhaus et Hocine Oumeraci. « BONDED POROUS REVETMENTS – EFFECT OF POROSITY ON WAVE-INDUCED LOADS AND HYDRAULIC PERFORMANCE ». Coastal Engineering Proceedings 1, no 33 (25 octobre 2012) : 45. http://dx.doi.org/10.9753/icce.v33.structures.45.

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The porosity and roughness of bonded revetments are both crucial for the hydraulic performance and the wave loading of the revetment and its foundation, and thus for the stability and durability of the entire structure. This is briefly shown by the selected results of a tentative comparative analysis of two large-scale test series performed in the Large Wave Flume (GWK) Hanover with two significantly different revetments: a highly porous and rough polyurethane bonded aggregate (PBA) revetment and an almost impermeable and relatively smooth interlocked pattern placed block (IPPB) revetment. These results motivated the initiation of the three years research project BoPoRe (Bonded Porous Revetments) which has the primary objective to investigate more systematically and separately the relative importance of both porosity and roughness for different slope steepnesses. This project is briefly introduced and the first results of preliminary scale model tests using 9 configurations for the porosity and roughness of the revetment subject to a wide range of wave conditions (surf similarity parameters 0.93-7.21) are briefly discussed.
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Sebastian Pap, J. zsef, Tom Schiefer et Irene Jansen. « Adhesively Bonded Structures withHybrid Yarn Textile-reinforced Plastics ». Journal of The Adhesion Society of Japan 51, s1 (2015) : 229–30. http://dx.doi.org/10.11618/adhesion.51.229.

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Wong, Ee-Hua, et Johan Liu. « Design Analysis of Adhesively Bonded Structures ». Polymers 9, no 12 (1 décembre 2017) : 664. http://dx.doi.org/10.3390/polym9120664.

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Potluri, P., E. Kusak et T. Y. Reddy. « Novel stitch-bonded sandwich composite structures ». Composite Structures 59, no 2 (février 2003) : 251–59. http://dx.doi.org/10.1016/s0263-8223(02)00087-9.

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Fournel, F., C. Martin-Cocher, D. Radisson, V. Larrey, E. Beche, C. Morales, P. A. Delean, F. Rieutord et H. Moriceau. « Water Stress Corrosion in Bonded Structures ». ECS Journal of Solid State Science and Technology 4, no 5 (2015) : P124—P130. http://dx.doi.org/10.1149/2.0031505jss.

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Thèses sur le sujet "Bonded structures"

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McConnell, Barry Kerr. « Dielectric studies of adhesively bonded structures ». Thesis, University of Strathclyde, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.426326.

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Graner, Solana Alejandro. « Fatigue initiation in adhesively bonded structures ». Thesis, University of Surrey, 2008. http://epubs.surrey.ac.uk/844365/.

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The objective of this research was to find patterns of fatigue initiation in adhesively bonded structures. Fatigue initiation plays a very important role in the useful life of any structure, but it is a difficult phenomenon to quantify. Three types of aluminium-FM73M single lap joints (SLJ) were tested in tensile mode at different loads. The damage was recorded using the backface strain technique. Six strain gauges (SGs) were installed to record damage. Several types of tests were performed: tests to failure, tests to limited damage and sectioning, and tests to limited damage and a residual strength test. The tests to failure were performed to obtain backface strain patterns. The specimens tested to limited damage were sectioned, polished and inspected under a microscope to study how the damage affected the adhesive. The tests to limited damage, followed by a static test to failure, were carried out to find the effect of damage on the static strength. The load-life data obtained matched previous data well. Experimental tests found that the damage appeared in the fillet as a microcrack formation, merging at the end of the test into a major crack. This pattern depended on geometry and load. The residual strength tests in specimens with limited damage showed that the joints kept a significant proportion of original static strength, even if the joint had been damaged significantly. Numerical simulations were performed in ABAQUS to match and predict fatigue life and backface strain patterns at different loads. Fortran was used to develop damage models based on user-defined field subroutines. Two elastic damage models were developed (one and two phase), which reduced the elastic modulus as damage increased. A more complete elasto-plastic damage model was also developed. In this model the elastic modulus and yield stress were reduced. This gave good predictions of both fatigue life and backface strain patterns. This model can be used to determine fatigue lives in other bonded structures and represents an important step forward in this area.
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Clark, Stewart. « Complex structures in tetrahedrally bonded semiconductors ». Thesis, University of Edinburgh, 1994. http://hdl.handle.net/1842/13420.

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Complex tetrahedral structures form good models for amorphous Group IV and III-V semiconductors. With a view of working towards examining non-crystalline materials, the structural, electronic and vibrational properties of complex tetrahedrally bonded semiconductors are investigated by various molecular dynamics techniques. First principles quantum mechanical molecular dynamics calculations are performed on two such structures and the effects of pressure on their behaviour is reported. A full free energy calculation using this method remains unfeasible and therefore an empirical bond charge model is used to calculate the full pressure-temperature phase diagram of the structures. Several surface reconstructions of a complex phase of silicon are then examined and the lowest energy surface of any silicon structure so far is found. Point defects in the diamond phase of silicon and carbon also give insight into various unusual bonding topologies that could be found in their amorphous phase. Structural and vibrational properties of several defects are considered. Finally, calculations on amorphous carbon and silicon at several densities are done and a comparison between the structural and electronic properties made. New bonding topologies are found in the structures including three centre bonding orbitals in the amorphous carbon models.
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White, Caleb, et caleb white@rmit edu au. « Health Monitoring of Bonded Composite Aerospace Structures ». RMIT University. Aerospace, Mechanical and Manufacturing Engineering, 2009. http://adt.lib.rmit.edu.au/adt/public/adt-VIT20090602.142122.

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Airframe assemblers have long recognised that for a new aircraft to be successful it must use less fuel, have lower maintenance requirements, and be more affordable. One common tactic is the use of innovative materials, such as advanced composites. Composite materials are suited to structural connection by adhesive bonding, which minimises the need for inefficient mechanical fastening. The aim of this PhD project was to investigate the application of existing, yet immature Structural Health Monitoring (SHM) techniques to adhesively bonded composite aerospace structures. The PhD study focused on two emerging SHM technologies - frequency response and comparative vacuum monitoring (CVM). This project aimed to provide missing critical information for each technique. This included determining sensitivity to damage, repeatability of results, and operating limitations for the frequency response method. Study of the CVM technique aimed to address effectiveness of damage detection, manufacture of sensor cavities, and the influence of sensor integration on mechanical performance of bonded structures. Experimental research work is presented examining the potential of frequency response techniques for the detection of debonding in composite-to-composite external patch repairs. Natural frequencies were found to decrease over a discrete frequency range as the debond size increased; confirming that such features could be used to both detect and characterise damage. The effectiveness of the frequency response technique was then confirmed for composite patch and scarf repair specimens for free-free and fixed-fixed boundary conditions. Finally, the viability of the frequency response technique was assessed for a scarf repair of a real aircraft component, where it was found that structural damping limited the maximum useable frequency. The feasibility of CVM technique for the inspection of co-cured stiffener-skin aircraft structures was explored. The creation of sensor cavities with tapered mandrels was found to significantly alter the microstructure of the stiffener, including crimping and waviness of fibres and resin-rich zones between plies. Representative stiffened-skin structure with two sensor cavity configurations (parallel and perpendicular to the stiffener direction) was tested to failure in tension and compression. While tensile failure strength was significantly reduced for both configurations (up to 25%), no appreciable differences in compression properties were found. Two potential sensor cavity configurations were investigated for the extension of the CVM technique to pre-cured and co-bonded scarf repair schemes. The creation of radial and circumferential CVM sensor cavities was found to significantly alter the microstructure of the adhesive bond-line and the architecture of the repair material in the case of the co-bonded repair. These alterations changed the failure mode and reduced the tensile failure strength of the repair. A fibre straightening mechanism responsible for progressive failure (specific to co-bonded repairs with circumferential cavities) was identified, and subsequently supported with acoustic emission testing and numerical analysis. While fatigue performance was generally reduced by the presence of CVM cavities, the circumferential cavities appeared to retard crack progression, reducing sensitivity to the accumulation of fatigue damage. These outcomes have brought forward the implementation of SHM in bonded composite structures, which has great potential to improve the operating efficiency of next generation aircraft.
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Keat, Loh Wei. « Modelling interfacial degradation in adhesively bonded structures ». Thesis, University of Surrey, 2002. http://epubs.surrey.ac.uk/798102/.

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Guyott, C. C. H. « The non-destructive testing of adhesively bonded structures ». Thesis, Imperial College London, 1987. http://hdl.handle.net/10044/1/38341.

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Thornton, Peter James. « Interlocked structures based on h-bonded barbiturate complexes ». Thesis, University of Birmingham, 2015. http://etheses.bham.ac.uk//id/eprint/5985/.

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The work contained within this thesis concerns the synthesis and characterisation of novel [2]-rotaxanes, mediated via H-bonded templation. The template in question is based upon the barbiturate receptor as developed by A. D. Hamilton which up until now had not been utilised in the synthesis of interlocked structures. The initial approaches centred on the use of long appendages of the barbiturate towards a threading, and subsequent clipping approach; however a lack of initial threading event prevented formation of the pseudorotaxane. In an attempt to overcome these difficulties, the synthesis of more rigid, dumbbell-barbiturates, were applied towards a receptor-based clipping approach, but the steric bulk acquired from the rigid spacer groups appeared to hinder any cyclisation. To overcome the problem of threading, shorter appendages were utilised and the threading was observed via a crystal structure of the complex. Subsequent stoppering of the azideterminated appendages in a CuAAC reaction afforded the first Hamilton Receptor based [2]- rotaxane. Further studies involving bichromophoric, anthracene-terminated receptors were then utilised with these barbiturate guests in the synthesis of a [2]-rotaxane via a novel light-induced photodimerisation.
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Meneghin, Ivan <1979&gt. « Bonded structures for enhanced damage tolerant pressurized fuselages ». Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2009. http://amsdottorato.unibo.it/1682/.

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Adhesive bonding provides solutions to realize cost effective and low weight aircraft fuselage structures, in particular where the Damage Tolerance (DT) is the design criterion. Bonded structures that combine Metal Laminates (MLs) and eventually Selective Reinforcements can guarantee slow crack propagation, crack arrest and large damage capability. To optimize the design exploiting the benefit of bonded structures incorporating selective reinforcement requires reliable analysis tools. The effect of bonded doublers / selective reinforcements is very difficult to be predicted numerically or analytically due to the complexity of the underlying mechanisms and failures modes acting. Reliable predictions of crack growth and residual strength can only be based on sound empirical and phenomenological considerations strictly related to the specific structural concept. Large flat stiffened panels that combine MLs and selective reinforcements have been tested with the purpose of investigating solutions applicable to pressurized fuselages. The large test campaign (for a total of 35 stiffened panels) has quantitatively investigated the role of the different metallic skin concepts (monolithic vs. MLs) of the aluminum, titanium and glass-fiber reinforcements, of the stringers material and cross sections and of the geometry and location of doublers / selective reinforcements. Bonded doublers and selective reinforcements confirmed to be outstanding tools to improve the DT properties of structural elements with a minor weight increase. However the choice of proper materials for the skin and the stringers must be not underestimated since they play an important role as well. A fuselage structural concept has been developed to exploit the benefit of a metal laminate design concept in terms of high Fatigue and Damage Tolerance (F&DT) performances. The structure used laminated skin (0.8mm thick), bonded stringers, two different splicing solutions and selective reinforcements (glass prepreg embedded in the laminate) under the circumferential frames. To validate the design concept a curved panel was manufactured and tested under loading conditions representative of a single aisle fuselage: cyclic internal pressurization plus longitudinal loads. The geometry of the panel, design and loading conditions were tailored for the requirements of the upper front fuselage. The curved panel has been fatigue tested for 60 000 cycles before the introduction of artificial damages (cracks in longitudinal and circumferential directions). The crack growth of the artificial damages has been investigated for about 85 000 cycles. At the end a residual strength test has been performed with a “2 bay over broken frame” longitudinal crack. The reparability of this innovative concept has been taken into account during design and demonstrated with the use of an external riveted repair. The F&DT curved panel test has confirmed that a long fatigue life and high damage tolerance can be achieved with a hybrid metal laminate low weight configuration. The superior fatigue life from metal laminates and the high damage tolerance characteristics provided by integrated selective reinforcements are the key concepts that provided the excellent performances. The weight comparison between the innovative bonded concept and a conventional monolithic riveted design solution showed a significant potential weight saving but the weight advantages shall be traded off with the additional costs.
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Gawith, Corin B. E. « Novel active waveguide devices in direct-bonded structures ». Thesis, University of Southampton, 2002. https://eprints.soton.ac.uk/15488/.

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This thesis describes a series of experimental studies on the use of direct bonding for optical waveguide fabrication. The direct bonding technique involves contacting two ultra-clean polished surfaces to form an adhesive-free vacuum-tight bond. Optical materials bonded in this way can be formed into waveguide devices, and this work extends direct bonding to include periodically poled materials and a new solid-state ion-exchange process. The first result of this work describes the fabrication of a 5.5-mm-long, 12-µm-thick periodically poled LiNbO3 planar waveguide buried in LiTaO3. Frequency doubling experiments performed with this device demonstrate a conversion efficiency of 4.3 %W-1, a value 40% greater than that calculated for an optimised bulk device of similar length. Also demonstrated is a photorefractive iron-doped LiNbO3 waveguide buried in non-photorefractive magnesium-doped LiNbO3. In optical limiting experiments this device demonstrates a change in optical density of 2 and photorefractive response time of 5 milliseconds, representing 20 times greater optical limiting and 60 times faster operational speed than the bulk material. K+-Na+ ion-exchange between direct-bonded glass layers is studied and used as a novel solid-state technique for waveguide fabrication. This process is also developed to incorporate direct-UV-written channel waveguides in an ion-exchanged buried photosensitive glass layer. Finally, operation of a single-mode channel waveguide laser in neodymium-doped photosensitive SGBN glass (based on a composition of silica, germania, boron, and sodium) is demonstrated, with propagation losses of < 0.3 dB cm-1 and milliwatt-order lasing thresholds.
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Burke, Nichola Jayne. « Hydrogen-bonded layer structures based on guanidinium sulfonates ». Thesis, University of Bath, 2005. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.413915.

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Livres sur le sujet "Bonded structures"

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Li, Zhan-Ting, et Li-Zhu Wu, dir. Hydrogen Bonded Supramolecular Structures. Berlin, Heidelberg : Springer Berlin Heidelberg, 2015. http://dx.doi.org/10.1007/978-3-662-45756-6.

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A, Baker A. Bonded Repair of Aircraft Structures. Dordrecht : Springer Netherlands, 1988.

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Baker, A. A., et R. Jones, dir. Bonded Repair of Aircraft Structures. Dordrecht : Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2752-0.

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Zilch, Konrad, Roland Niedermeier et Wolfgang Finckh, dir. Strengthening of Concrete Structures with Adhesively Bonded Reinforcement. Berlin, Germany : Wilhelm Ernst & Sohn, Verlag für Architektur und technische Wissenschaften GmbH & Co. KG, 2014. http://dx.doi.org/10.1002/9783433604014.

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Khalil, Abouelmakarem Ahmed. Static analysis of bonded structures with double containment joints. Birmingham : University of Birmingham, 1985.

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Broughton, James G. Performance enhancement of structures by means of bonded reinforcement. Oxford : Oxford Brookes University, 1998.

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Rahimi, Hamid. Strengthening of concrete structures with externally bonded fibre-reinforced plastics. Oxford : Oxford Brookes University, 1996.

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Aruleswaran, Arulnageswaran. Dynamic behaviour of adhesive bonded sub-assemblies for automotive vehicle structures. Oxford : Oxford Brookes University, 2001.

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Qian, Duan. The development of two dimensional mixed finite elements for bonded joint structures. [Downsview, Ont.] : Aerospace Science and Engineering, 1985.

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Institute, American Concrete, dir. Guide for the design and construction of externally bonded FRP systems for strengthening concrete structures. Farmington Hills, Mich : American Concrete Institute, 2008.

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Chapitres de livres sur le sujet "Bonded structures"

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Delgrange, G., et J. C. Ehrström. « Recent Development on Bonded Structures ». Dans ICAF 2011 Structural Integrity : Influence of Efficiency and Green Imperatives, 93–104. Dordrecht : Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-1664-3_7.

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Vittal, Jagadese J. « Hydrogen-bonded Coordination Polymeric Structures ». Dans Frontiers in Crystal Engineering, 297–319. Chichester, UK : John Wiley & Sons, Ltd, 2006. http://dx.doi.org/10.1002/0470022612.ch12.

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Mayton, D. J., et James W. Wagner. « Electromagnetic Stressing of Bonded Structures ». Dans Review of Progress in Quantitative Nondestructive Evaluation, 1107–14. Boston, MA : Springer US, 1993. http://dx.doi.org/10.1007/978-1-4615-2848-7_142.

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Kanterakis, Georgios, Roland Chemama et Konstantinos Kitsianos. « Bonded Repair of Composite Structures ». Dans Revolutionizing Aircraft Materials and Processes, 359–92. Cham : Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-35346-9_13.

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Lees, W. A. « A Review—The Design and Assembly of Bonded Composites ». Dans Composite Structures, 471–506. Dordrecht : Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3662-4_36.

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Marr, G. R., R. P. Barrowcliffe et A. R. Curtis. « The Non-destructive Evaluation of Composite Bonded Joints ». Dans Composite Structures 3, 502–10. Dordrecht : Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-4952-2_35.

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Veyhl, Christoph, Rolf Winkler, Markus Merkel et Andreas Öchsner. « Structural Characterisation of Diffusion-Bonded Hollow Sphere Structures ». Dans Defect and Diffusion Forum, 105–12. Stafa : Trans Tech Publications Ltd., 2008. http://dx.doi.org/10.4028/3-908451-62-0.105.

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Reinhart, Theodore J. « Surface treatments for bonded repair of metals ». Dans Bonded Repair of Aircraft Structures, 19–30. Dordrecht : Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2752-0_2.

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Hart-Smith, L. John. « Adhesively Bonded Joints in Aircraft Structures ». Dans Handbook of Adhesion Technology, 1101–47. Berlin, Heidelberg : Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-01169-6_44.

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Hart-Smith, L. John. « Adhesively Bonded Joints in Aircraft Structures ». Dans Handbook of Adhesion Technology, 1–50. Cham : Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-42087-5_44-2.

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Actes de conférences sur le sujet "Bonded structures"

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Summers, James, Fredrick R. Rutz et Carnot Nogueira. « Shear Strength of Bonded Concrete ». Dans Structures Congress 2020. Reston, VA : American Society of Civil Engineers, 2020. http://dx.doi.org/10.1061/9780784482896.038.

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

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Selvarathinam, Alex S., et Carl Rouseau. « Practical Bonded Joint Stress Analysis ». Dans 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston, Virginia : American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-2067.

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null. « Inspection of bonded structures at Rolls-Royce ». Dans IEE Colloquium on Techniques for the Inspection of Bonded Structures. IEE, 1997. http://dx.doi.org/10.1049/ic:19970054.

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Zeng, Q., et C. Sun. « A new bonded composite wavy lap joint ». Dans 41st Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina : American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-1484.

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KAN, H., et M. RATWANI. « Analysis of step-lap joint with weakly bonded regions ». Dans 26th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-825.

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Bogdanovich, Alexander, Indrajith Kizhakkethara, Alexander Bogdanovich et Indrajith Kizhakkethara. « Three-dimensional finite element analysis of adhesively bonded plates ». Dans 38th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1120.

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Rastogi, Naveen, B. Deepak, Som Soni, Naveen Rastogi, B. Deepak et Som Soni. « Stress analysis codes for bonded joints in composite structures ». Dans 38th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1341.

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Hassanen, Mahmoud A. H., et Mohammed Raoof. « R.C. Beams Upgraded with Externally Bonded Plates ». Dans Structures Congress 2000. Reston, VA : American Society of Civil Engineers, 2000. http://dx.doi.org/10.1061/40492(2000)183.

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Naboulsi, S., S. Mall, S. Naboulsi et S. Mall. « Analysis of cracked metallic structure with imperfectly bonded composite patch ». Dans 38th Structures, Structural Dynamics, and Materials Conference. Reston, Virigina : American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1363.

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Rapports d'organisations sur le sujet "Bonded structures"

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Monson, Peter A. Modeling Adsorption of Hydrogen-Bonded Molecules in Porous Structures. Fort Belvoir, VA : Defense Technical Information Center, février 2005. http://dx.doi.org/10.21236/ada430464.

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Hudson, Bruce S. ''Inelastic Neutron Scattering and Periodic Density Functional Studies of Hydrogen Bonded Structures''. Office of Scientific and Technical Information (OSTI), octobre 2004. http://dx.doi.org/10.2172/833891.

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Clearfield, Abraham. The Synthesis, Structures, and Chemical Properties of Macrocyclic Ligands Covalently Bonded into Layered Arrays. Office of Scientific and Technical Information (OSTI), novembre 2014. http://dx.doi.org/10.2172/1164084.

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Abraham Clearfield. The Synthesis, Structures and Chemical Properties of Macrocyclic Ligands Covalently Bonded into Layered Arrays. Office of Scientific and Technical Information (OSTI), juillet 2009. http://dx.doi.org/10.2172/959123.

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Riveros, Guillermo, Felipe Acosta, Reena Patel et Wayne Hodo. Computational mechanics of the paddlefish rostrum. Engineer Research and Development Center (U.S.), septembre 2021. http://dx.doi.org/10.21079/11681/41860.

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Purpose – The rostrum of a paddlefish provides hydrodynamic stability during feeding process in addition to detect the food using receptors that are randomly distributed in the rostrum. The exterior tissue of the rostrum covers the cartilage that surrounds the bones forming interlocking star shaped bones. Design/methodology/approach – The aim of this work is to assess the mechanical behavior of four finite element models varying the type of formulation as follows: linear-reduced integration, linear-full integration, quadratic-reduced integration and quadratic-full integration. Also presented is the load transfer mechanisms of the bone structure of the rostrum. Findings – Conclusions are based on comparison among the four models. There is no significant difference between integration orders for similar type of elements. Quadratic-reduced integration formulation resulted in lower structural stiffness compared with linear formulation as seen by higher displacements and stresses than using linearly formulated elements. It is concluded that second-order elements with reduced integration and can model accurately stress concentrations and distributions without over stiffening their general response. Originality/value – The use of advanced computational mechanics techniques to analyze the complex geometry and components of the paddlefish rostrum provides a viable avenue to gain fundamental understanding of the proper finite element formulation needed to successfully obtain the system behavior and hot spot locations.
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Knowlton, W. B. Structural and phonon transmission study of Ge-Au-Ge eutectically bonded interfaces. Office of Scientific and Technical Information (OSTI), juillet 1995. http://dx.doi.org/10.2172/106618.

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Liu, Cheng-Hsin, Ha L. Nguyen et Omar M. Yaghi. Reticular Chemistry and Harvesting Water from Desert Air. AsiaChem Magazine, novembre 2020. http://dx.doi.org/10.51167/acm00007.

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Although chemists, in general, are concerned with the art and science of constructing molecules and understanding their behavior, for a long time the idea that such molecules can be linked together by strong bonds to make infinite, extended structures were fraught with failure. The notion of using molecular building blocks to make such structures invariably led to chaotic, ill-defined materials and therefore not only defying the chemists’ need to exert their will on the design of matter but also preventing them from deciphering the atomic arrangement of such products. The field remained undeveloped for most of the twentieth century, and it was taken as an article of faith that linking molecules by strong bonds to make extended structures is a “waste of time” because “it doesn’t work.”
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Roach, D., et P. Walkington. Full-Scale Structural and NDI Validation Tests of Bonded Composite Doublers for Commercial Aircraft Applications. Office of Scientific and Technical Information (OSTI), février 1999. http://dx.doi.org/10.2172/4368.

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Diebold, Francis, et Canlin Li. Forecasting the Term Structure of Government Bond Yields. Cambridge, MA : National Bureau of Economic Research, octobre 2003. http://dx.doi.org/10.3386/w10048.

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Pribyl, Zachary Jerome. Structural Health Monitoring of Epoxy Bond between Dissimilar Materials. Office of Scientific and Technical Information (OSTI), décembre 2019. http://dx.doi.org/10.2172/1578015.

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