Relevant bibliographies by topics / Riveted

Academic literature on the topic 'Riveted'

Author: Grafiati
Published: 7 July 2024
Last updated: 7 July 2024

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

Journal articles on the topic "Riveted":

1

Dourado, Marco Daniel Malheiro, and José Filipe Bizarro de Meireles. "A Simplified Finite Element Riveted Lap Joint Model in Structural Dynamic Analysis." Advanced Materials Research 1016 (August 2014): 185–91. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.185.

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This paper proposes a simplified finite element model to represent a riveted lap joint in structural dynamic analysis field. The rivet is modeled byspring-damperelements. Several numerical models are studied with different quantities of rivets (1, 3 and 5) andspring-damperelements (4, 6, 8, 12, 16 and 20) per rivet. In parallel, samples of two aluminum material plates connected by different quantities of rivets (1, 3 and 5) are built and tested in order to be known its modal characteristics – natural frequencies and mode shapes. The purpose of the different settings is to get the best numerical riveted lap joint representation relatively to the experimental one. For this purpose a finite element model updating methodology is used. An evaluation of the best numerical riveted lap joint is carried out based on comparisons between the numerical model after updating and the experimental one. It is shown that the riveted lap joints composed by eight and twelvespring-damperelements per rivet have the best representation. A stiffness constant valuekis obtained for the riveted lap joints in study.
2

Witek, Lucjan, and Monika Lubas. "Experimental Strength Analysis of Riveted Joints Using Blind Rivets." Journal of KONES 26, no. 1 (March 1, 2019): 199–206. http://dx.doi.org/10.2478/kones-2019-0024.

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Abstract This article presents results of experimental investigations of the lap blind riveted joint. The main goal of the work is determination of destructive load of the blind riveted joints. The blind rivets were originally used in the aircraft structures where access to both sides of the riveted structure is impossible. Blind rivets are now commonly used in many branches of industry because of their low cost. Moreover, the riveting process is uncomplicated. There are many publications about analysis of strength of solid rivets in the research literature. However, the strength analysis of the blind rivets was rarely undertaken. There is the research gap in the analysis of both the strength and the load capacity of blind riveted joints. The influence of selected geometrical parameters of the joint on the stress distribution and the destructive force was not widely described in literature. The first part of the work presents a review of standards and publications related to stress and strength analysis of blind riveted joints. The next part of the study describes experimental investigations of joints. The examined specimens were made out of AW 2017 aluminum alloy, cut from 1 [mm] thick sheet. Investigated blind rivets were made out of aluminum alloy. The lap joint with one rivet and the single row five-rivet joint were investigated. Moreover, the different size of hole chamfer were considered. The experimental tests were performed with the use of Zwick-Roell tension machine. The main results of experimental investigations are ultimate shear load diagrams. The influence of both the hole chamfer and the number of rivets on destructive force and shear diagrams of blind riveted joints were in detail analysed. After shear tests, the fractured rivets were magnified in order to explain the failure phenomenon of blind rivets. In the future research works the obtained results will be used in strength analysis of the blind riveted joints using the finite element method.
3

Yu, Haidong, Bin Zheng, Xun Xu, and Xinmin Lai. "Residual stress and fatigue behavior of riveted lap joints with various riveting sequences, rivet patterns, and pitches." Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture 233, no. 12 (March 8, 2019): 2306–19. http://dx.doi.org/10.1177/0954405419834481.

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The residual stress of multi-rivet structures is related with the riveting sequence, the rivet pattern, and the pitch due to the deformation interaction of different rivets. The stress amplitude of riveted structures subjected to the cyclic loads is affected by the residual stress, which increases the difficulty in the prediction of fatigue life. In this article, the riveting processes for single-row and triple-row riveted lap joints with various riveting sequences, rivet patterns, and pitches are studied numerically and experimentally. The residual stresses for both types of riveted structures are verified by the testing data. Significant difference appears in the residual stress field for riveted lap joints with various riveting sequences and rivet patterns. The decrease in the rivet pitch increases the compressive residual stress at the edge of the rivet hole. Furthermore, the fatigue life prediction model is developed for multi-rivet structures, in which the coupling effect of residual stress and cyclic load is considered. The fatigue experiments are conducted for riveted lap joints with various riveting sequences, rivet patterns, and pitches. The accuracies of the numerical results obtained from the Homan model and the developed model are compared with the experimental data. The proposed fatigue model shows better performance to predict fatigue life for multiple rivet structures.
4

Kang, Yonggang, Huan Xiao, Zihao Wang, Guomao Li, and Yonggang Chen. "Three-Dimensional Characterization of Residual Stress in Aircraft Riveted Panel Structures." Aerospace 11, no. 7 (July 4, 2024): 552. http://dx.doi.org/10.3390/aerospace11070552.

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The residual stress field induced by interference-fit riveting in aircraft panel structures significantly affects the fatigue performance around the rivet holes. Common residual stress analytical models often overlook the non-uniformity of interference between the rivet and the hole, which impacts the applicability of these models. Addressing this issue, an analytical model of residual stress around the rivet hole is proposed for a typical single-riveted structure based on the thick-walled cylinder theory and Lame’s equations, considering the non-uniform interference along the axis of the rivet hole. This novel model is then extended to multi-riveted structures in fuselage panels. Using vector synthesis, analytical models for single-row double-rivets and double-row quadruple-rivets configurations were derived. The established analytical models provide a three-dimensional characterization of the residual stress field in typical riveted structures. Finally, the accuracy of the model is verified through X-ray diffraction experiments and FEM simulation results.
5

Lis, Zbigniew, and Adam Lipski. "Evaluation of the Riveted Joint Load-Carrying Capacity Based on the Formed Rived Head Dimension." Solid State Phenomena 224 (November 2014): 261–66. http://dx.doi.org/10.4028/www.scientific.net/ssp.224.261.

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The formed rivet head was measured in order to verify rivet closing-up forcein the executed riveted joint. The measurements were performed using two specimen series with strapped joint. The first series of specimens was prepared using standard riveting technology: drilling and reaming of holes and kinematic heading of rivets. In the second series of specimens modified technology was used: drilling, sizing and heading of rivets with controlled heading force.The relationship of the formed rivet head diameter on the heading force was determined. For that purpose tests with controlled heading force were performed and the formed rivet head diameter for each force was measured. The limits of formed rivet head diameter for the second series of specimens, which were headed using controlled heading force were calculated. Based on the scatter of formed rivet head diameters for the first series of specimens the range of forces achieved during kinematic heading of rivets was determined. The riveted joint load-carrying capacity using tension was assumed. Special instrumentation was prepared for riveted joint tests. Achieved joint load-carrying capacity results were collated with specific heading forces for the first series of specimens. Based on the heading force values put on the load-carrying capacity diagram was concluded that kinematic heading does not guarantee achievement of the optimum load-carrying capacity.
6

Ren, Kerong, Haobing Han, Wentao Xu, and Hua Qing. "The Effect of Rivet Arrangement on the Strengths of Lap Joints and Lap Joint Design Methods." Applied Sciences 13, no. 9 (May 3, 2023): 5629. http://dx.doi.org/10.3390/app13095629.

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To address the impact of rivet arrangement on the strengths of riveted lap joints, the failure modes and failure mechanisms of riveted lap joints were first studied using finite element analysis software. Next, the effects of the number of rivets, rivet rows, rivet arrangement, and row spacing on the lap joint strength were studied using the peak load as the evaluation index. Then, we proposed the concept of line load density to solve the problem that a varying rivet spacing and rivet edge distance will change the width of the sheet and thus the maximum load capacity, which is used as an index to study the effect of rivet spacing and rivet edge distance on the lap strength. Finally, a spring–mass model was developed to study the forces present in multi-row riveting. The model could accurately calculate the force–displacement curves during tensioning. The results show that when multiple rivet rows are used, higher stress concentrations cause the plate to first fracture at an outer rivet row with more rivets; therefore, the rivets should be arranged such that there are more rivets in the middle and fewer rivets on both sides. When the total rivet strength is greater than the remaining strength of the plate, the numbers of rivets and rivet rows have limited effects on the lap joint strength; however, this primarily affects the damaged form of the lap joint member. When the rivet spacing is less than 5d, the lap strength increases with increases in the rivet spacing, and when the rivet spacing is greater than 5d, the lap strength does not change significantly with increases in the rivet spacing. When the rivet edge distance is less than 3d, the lap joint strength increases with increases in the rivet edge distance, and when the rivet edge distance is greater than 3d, it has a limited effect on the lap joint strength. The rivet row spacing has no significant effect on the lap joint strength. The results of this study are valuable for improving the strengths of riveted structures in aircraft.
7

Rudawska, Anna, Izabela Miturska, Dana Stančeková, and Jacek Mucha. "The strength of traditional and self-pierced riveted joints." MATEC Web of Conferences 244 (2018): 01007. http://dx.doi.org/10.1051/matecconf/201824401007.

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The objective of this study is to compare the strength of riveted joints fabricated by traditional riveting (with pre-drilled holes) and self-piercing riveting (SPR) for different types of joints. Riveted joints were produced using steel and aluminum alloy rivets and two types of sheet material: 235JR steel sheet and EN AW 6060 aluminum alloy sheet with the following dimensions: length l = 100 ± 1 mm, width b = 50 ± 1 mm and thickness g = 2 mm. For all tested types of riveted joints (pre-drilled and SPR), 5 sets of joints were fabricated, each set containing 6 samples. The sets of joints differed with respect to the number of rivets (1, 2, 3, 4 and 6 rivets), joint type (single-, three- and four-riveted joints) and lap length. For all tested joints, the highest load capacity was obtained for self-pierced riveted joints, while the lowest - for pre-drilled joints with aluminum alloy rivets. In addition, it was found that the shear strength of self-pierced riveted joints is higher than that of aluminum and steel blind rivets.
8

Livieri, Paolo. "Numerical Analysis of Double Riveted Lap Joints." Lubricants 11, no. 9 (September 12, 2023): 396. http://dx.doi.org/10.3390/lubricants11090396.

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In a previous work, the fatigue behaviour of different hot riveted joints under fatigue loadings were experimentally calculated. In particular, the experimental data showed a Wöhler curve slope close to five against the slope of three proposed by Eurocode 3. However, two series of shear splice riveted joints showed, at two million cycles, a stress range very close to the value suggested by Eurocode for shear splices that use non-preloaded high-strength bolts. In order to clarify the fatigue behaviour of riveted joints at high- and medium-fatigue regimes, this paper presents a preliminary three-dimensional non-linear FE analysis of a double-riveted lap joint previously analysed experimentally. Different friction coefficients and rivet clamping stress have been taken Into account, as well as the elastoplastic behaviours of the main plate subjected to tensile loadings. The numerical analysis shows that the friction force tends to reduce the range of stresses at the net section during fatigue loadings, and the force distribution or the stress concentration on the rivets is always critical for the external rivet, which is also the case regarding the non-linear behaviour of the material.
9

Liu, Jintong, Anan Zhao, Zhenzheng Ke, Zhendong Zhu, and Yunbo Bi. "Influence of Rivet Diameter and Pitch on the Fatigue Performance of Riveted Lap Joints Based on Stress Distribution Analysis." Materials 13, no. 16 (August 16, 2020): 3625. http://dx.doi.org/10.3390/ma13163625.

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Interference-fit riveting is one of the most widely used mechanical joining ways in aircraft assembly. The fatigue performance of riveted joints has a significant impact on the service life and reliability of aircraft. In this paper, the fatigue performance of the riveted lap joints with various rivet diameters and pitches are studied based on stress distribution analysis under tensile load. First, a theoretical model of the riveted lap joint under tensile load is developed by using the spring-mass model. The rivet-load stress, bypass stress, and interference stress around the riveted hole are analyzed. Then, the finite element (FE) model of riveted lap joints are established. The influence of rivet diameter and pitch on stress distribution around the riveted hole are discussed. Finally, the fatigue tests are conducted with riveted lap joint specimens to verify the theoretical model and FE results, and a good agreement is observed. Based on the simulation and experimental results, a good combination of structural parameters of the riveted lap joint is found which can optimize the stress distribution around the riveted hole and improve the fatigue life of the riveted lap joint.
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Fortier, Vincent, Jean-E. Brunel, and Louis L Lebel. "Fastening composite structures using braided thermoplastic composite rivets." Journal of Composite Materials 54, no. 6 (August 14, 2019): 801–12. http://dx.doi.org/10.1177/0021998319867375.

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Aerospace composite material components are currently joined using heavy titanium bolts. This joining method is not ideal when considering its weight, thermal expansion, electrical conductivity, and risk of unbalanced load distribution. We propose here an innovative fastening technology using thermoplastic composite rivets. A rivet blank is heated above its melting temperature using Joule heating and is formed directly in the composite laminates by an automated process. Carbon fiber and polyamide blanks were used with two fiber architecture: 2D braid and unidirectional. The braided architecture showed superior manufacturing performance and repeatability. Joints were riveted in less than 40 s per rivet. The temperature measured in the riveted composite laminate in the vicinity of formed rivet reached only 136℃ during riveting. Double fastener lap shear testing showed breaking load of 6146 N per fastener. This joint strength is higher than comparable aluminum-riveted joints, and the specific joint strength is higher than titanium-bolted joints. With these advantages, the technology could be developed and used in the next generations of lighter, cleaner, and safer aircraft.
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Journal articles Dissertations / Theses Books

Dissertations / Theses on the topic "Riveted":

1

Imam, Boulent. "Fatigue analysis of riveted railway bridges." Thesis, University of Surrey, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.431074.

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Kecelioglu, Galip. "Stress And Fracture Analysis Of Riveted Joints." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/12610132/index.pdf.

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The objective of this study is to model and analyze a three dimensional single riveted lap joint (with and without a crack). By using finite element method, stress and fracture analyses are carried out under both the residual stress field and external tensile loading. Using a two step simulation, riveting process and subsequent tensile loading of the lap joint are simulated to determine the residual and overall stress state. Residual stress state due to riveting is obtained by interference and clamping misfit method. By employing different interference and clamping misfit values, the effects of riveting process parameters on stress state are examined. Two cracks namely the semi elliptical surface crack at faying surfaces of plates and the quarter elliptical corner crack at rivet hole are the most widely observed crack types in riveted joints. Fracture analysis of cracked riveted joints is carried out by introducing these two crack types to the outer plate at a plane perpendicular to the loading. The mixed mode stress intensity factors (SIFs) and energy release rates (G) around the crack front are obtained by using displacement correlation technique (DCT). Effects riveting process parameters (interference and clamping ratios) and geometrical parameters (crack shape and size) on fracture parameters are studied. The stress intensity factor solutions presented herein could be useful for correlating fatigue crack growth rates, fracture toughness computation, and multiple site damage (MSD) analysis in aircraft bodies.
3

Garcia, Abilio Neves. "Multiple site damage of aeronautical riveted joints." Thesis, Cranfield University, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.427165.

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Kim, Jueseok. "Linear Finite Element Modeling of Joined Structures with Riveted Connections." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1563273473791073.

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Han, Li. "Mechanical behaviour of self-piercing riveted aluminium joints." Thesis, University of Hertfordshire, 2003. http://hdl.handle.net/2299/14159.

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The introduction of alternative materials and in particular aluminium alloys, for vehicle body applications has impelled the development of new joining techniques. Traditional joining methods such as spot-welding and arc-welding are being challenged. Self-piercing riveting has attracted considerable interest by the automotive industry and has been used as an alternative to spot-welding in vehicle body assembly. However, self-piercing riveting is a relatively new joining method and as such it is not well understood. The aim of this project was therefore to develop an understanding of the mechanical behaviour of self-piercing riveted joints. The effects of paint-baking, shelf-life, pre-straining and surface condition of the sheet material on the joint quality and behaviour were therefore examined. Aluminium alloy sheet materials, 5754 and AA6111, were used in this investigation. The project began with a metallographic inspection of cross-sections of samples that were joined under different conditions in order to examine the effect of process variables on the joint quality. This part of the investigation led to the identification of suitable setting parameters that produced joints which, by metallographic inspection, were of good quality. It was also observed that some process variables, such as sheet thickness combination, rivet and die design and setting force, affected the joint quality and therefore needed to be taken into consideration in the choice of the processing parameters. Subsequent work focused on mechanical testing. Lap shear, T-peel, pull-out and fatigue tests were carried out in order to examine the mechanical behaviour and to analyse the failure mechanisms of the joints. The work showed that the strength, the thickness and the surface condition of the riveted sheets affected the strength and the failure mechanisms of the joints. The joint strength was also observed to be dependent on the rivet and anvil design as well as the setting force. In addition, the joint strength and behaviour differed as the specimen geometry thus emphasising the need for a test standard for self-piercing riveted joints. Paint baking led to a marginal and insignificant reduction in the static strength, whilst resulting in a reduction in the fatigue strength of the joints as a consequence of recovery of the 5754 alloy and the removal of the wax-based surface lubricant. The effect of 3%, 5% and 10% pre-straining of the 5754 sheet on the quality and performance of the self-piercing riveted joints was also examined. It was established that it was possible to produce joints of good quality, higher strength and superior fatigue performance by using the same setting parameters as for joints without additional pre-straining. An investigation of the effect of the shelf-life of AA6111 indicated that this only had a minor and insignificant effect on the joint quality and behaviour. It was therefore deduced that the quality and performance of joints would not be compromised even after an AA6111 self-life of 21 months. The effect of the interfacial characteristics on the joint quality and behaviour was examined by placing a PTFE layer at the interface between the riveted sheets. It was observed that the PTFE insert significantly reduced the joint strength and changed the failure mechanism. Three distinct failure modes, referred to as rivet pull-out, rivet fracture and sheet material failure, were observed during this investigation. All shear tested samples failed by rivet pull-out. The same failure mechanism was the only one observed for the pull-out tests. The failure mechanism for the peel test depended on the thickness of the rivet sheet. For joints with a (1 mm+2mm)/(0.9mm+2mm) combination, fracture of the thinner sheet material dominated the failure mechanism, whilst for joints with a (2mm+2mm) combination, rivet pull-out was the only failure system. Rivet fracture and sheet material failure were also observed during fatigue testing. Examination of samples following fatigue testing led to the observation of fretting which had not been reported by previous investigators working with self-piercing rivets. Fretting had an important effect on the fatigue strength and fatigue failure mechanisms. Inspection of fatigue fractured samples which were tested at maximum applied loads ranging from 50% to 85% of the ultimate shear load of the joints exhibited fretting scars at three different interfaces. Flange-face fretting was observed to take place at one side of the interface between the two riveted sheets and led to the formation of mainly A1203 debris. Pin-bore fretting was observed to occur between the rivet shank and the aluminium alloy sheet and led to debris containing oxides of aluminium and iron together with the oxides of zinc and tin from the wear of the corrosion protective coating of the rivet. Both types of fretting were affected by the applied load and the surface condition of the riveted sheets. Further examination indicated that fretting contributed to the initiation and propagation of fatigue cracks. The failure modes during fatigue testing were affected by the fretting behaviour and were dependent on the applied load and the interfacial conditions. A PTFE layer introduced a very low coefficient of friction leading to a significantly reduction in the amount of fretting. However, this was accompanied with a change in the load transfer mechanism resulting in rivet fracture and a shorter fatigue life. The paint-baking process led to the removal of the wax-based surface lubricant and fretting cracks therefore initiated at an earlier stage of the fatigue test. In addition, fretting also led to a significant work-hardening of the riveted sheets. It was observed that there was an increase in microhardness at the regions immediately below the fretting area from the riveted sheets. The depth of the work-hardened area below the fretting interface after different periods of fretting represented the depth of damage as a result of fretting fatigue. It was therefore further indicated that fretting played an important role in the fatigue behaviour and would probably affect the crash behaviour of the joints. The effect of secondary bending, an inherent feature of lap joints, was examined and analysed using strain gauge measurements. It was established that secondary bending contributed to the failure mechanism and led to a significant reduction in the fatigue strength of such joints. Using the experimental data an analysis has been carried out to predict the fatigue strength in the absence of secondary bending.
6

Abdulla, Warda Ibrahim. "FATIGUE BEHAVIOR AND SCALE EFFECTS IN RIVETED JOINTS." University of Akron / OhioLINK, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=akron161651595564376.

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7

Bejgum, Mahesh. "TESTING AND ANALYSIS OF HEAVY DUTY RIVETED GRATINGS." University of Akron / OhioLINK, 2006. http://rave.ohiolink.edu/etdc/view?acc_num=akron1154492162.

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8

Cinnam, Vikas Kumar Cinnam. "GRILLAGE ANALYSIS OF HEAVY-DUTY RIVETED STEEL GRATINGS." University of Akron / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=akron1525796487234452.

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9

Krishnappa, Uma Shankar. "Numerical investigation of self-piercing riveted dual layer joint." Thesis, Wichita State University, 2008. http://hdl.handle.net/10057/2105.

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Self-piercing riveting (SPR) is a high-speed mechanical fastening technique for point joining of sheet-material components. SPR is becoming important in automotive applications for aluminium vehicle body assembly. However, compared with current sheet-metal joining processes in the automotive industry, the effects of various parameters such as mechanical properties, rivet setting methods and systems, methods of removing self-piercing rivets, etc. A study examining the effect of specimen configuration on the mechanical behavior of self-piercing riveted, dual-layer joints in aluminium alloys was conducted. It has observed that the specimen configuration had a significant effect on the strength and failure mechanism of a self-piercing riveted dual-layer joint. The basic aspects of SPR process forming by conducting both explicit and implicit analysis have been investigated in this thesis. It was found that the operating force-deformation curve of SPR process was determined by the rivet deformation force and its displacement. Under certain process conditions, an increase in inertia effect due to high velocity of metal forming process results was not significant to an extent. In this research, the springback characteristic parameters of the SPR process were also studied. The springback analysis carried out at the end of the forming process showed that the dimensional change in the part due to springback was not significant.
Wichita State University, College of Engineering, Dept. of Mechanical Engineering
Includes bibliographic references (leaves 51-53)
10

Krishnappa, Uma Shankar Lankarani Hamid M. "Numerical investigation of self-piercing riveted dual layer joint." A link to full text of this thesis in SOAR, 2008. http://hdl.handle.net/10057/2105.

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Wichita State University, College of Engineering, Dept. of Mechanical Engineering.
Copyright 2008 by Uma Shankar Krishnappa. All Rights Reserved. Includes bibliographical references (leaves 51-53).
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Books on the topic "Riveted":

1

Brook, Meljean. Riveted. New York: Berkley Sensation, 2012.

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Brook, Meljean. Riveted. New York: Berkley Sensation, 2014.

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W, Wolfe Ronald, Stahl Doug, and Forest Products Laboratory (U.S.), eds. Timber rivet connections in U.S. domestic species. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 2004.

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DiBattista, Jeffrey D. Fatigue of riveted tension members. Edmonton: Dept. of Civil Engineering, University of Alberta, 1995.

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Wolfe, Ronald W. Timber rivets in structural composite lumber. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 2004.

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Skorupa, Andrzej, and Malgorzata Skorupa. Riveted Lap Joints in Aircraft Fuselage. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-4282-6.

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Åkesson, B. Fatigue life of riveted steel bridges. Boca Raton, Fla: CRC Press/Balkema, 2010.

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Adamson, Daniel Edward Joseph. Fatigue tests of riveted bridge girders. Edmonton, Canada: University of Alberta, Dept. of Civil Engineering, 1995.

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Åkesson, B. Fatigue life of riveted steel bridges. Boca Raton, Fla: CRC Press/Balkema, 2010.

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Young, C. R. The distribution of stress in riveted connections. [S.l: s.n., 1991.

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Book chapters on the topic "Riveted":

1

Hooijmeijer, P. A. "Riveted repairs." In Fibre Metal Laminates, 441–49. Dordrecht: Springer Netherlands, 2001. http://dx.doi.org/10.1007/978-94-010-0995-9_29.

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Josephs, Harold, and Ronald L. Huston. "Riveted and Bolted Joints." In Blake’s Design of Mechanical Joints, 135–76. Second edition. | Boca Raton: CRC Press, Taylor & Francis, 2019. | Series: Mechanical engineering | Revised edition of: Design of mechanical joints / Alexander Blake. c1985.: CRC Press, 2018. http://dx.doi.org/10.1201/9781315153827-5.

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Homan, J. J., R. P. G. Müller, F. Pellenkoft, and J. J. M. de Rijck. "Fatigue of riveted joints." In Fibre Metal Laminates, 173–95. Dordrecht: Springer Netherlands, 2001. http://dx.doi.org/10.1007/978-94-010-0995-9_12.

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Sheikhi, Mohammad Rauf, Melih Cemal Kuşhan, and Selim Gürgen. "Riveted Joints in Aircraft Structures." In Joining Operations for Aerospace Materials, 27–40. Cham: Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-59446-5_2.

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Atzeni, Eleonora, Rosolino Ippolito, and Luca Settineri. "FEM Modeling of Self-Piercing Riveted Joint." In Sheet Metal 2007, 655–62. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-437-5.655.

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Leape, Lucian L. "Enforcing : The Joint." In Making Healthcare Safe, 185–202. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-71123-8_12.

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AbstractOn March 30, 1981, Ronald Reagan, president of the USA, was shot in an assassination attempt. During his lifesaving surgery at the George Washington Hospital, the nation was riveted by the clear and calm account of its progress by the hospital’s physician spokesman, Dennis O’Leary. Five years later, O’Leary became the head of the Joint Commission on Accreditation of Hospitals.
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Altuntop, Elif, Murat Aykan, and Melin Şahin. "Parameter Identification of Riveted Joints Using Vibration Methods." In Shock & Vibration, Aircraft/Aerospace, and Energy Harvesting, Volume 9, 47–53. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-15233-2_6.

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Skorupa, Andrzej, and Małgorzata Skorupa. "Riveted Lap Joints in a Pressurized Aircraft Fuselage." In Solid Mechanics and Its Applications, 1–9. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-4282-6_1.

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He, Xiao Cong, Ian Pearson, and Ken W. Young. "Finite Element Analysis of Self-Pierce Riveted Joints." In Sheet Metal 2007, 663–68. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-437-5.663.

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Ivorra, S., B. Torres, D. Bru, and D. Camassa. "Dynamic Identification of a Historic Railway Riveted Bridge." In Lecture Notes in Civil Engineering, 68–77. Cham: Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-61421-7_7.

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Conference papers on the topic "Riveted":

1

Chen, Yu, Ryo Sakura, Takashi Yamaguchi, Gen Hayashi, Motoshi Yamauchi, and Keita Ueno. "Load transferring mechanism of long riveted joint partially replaced by high-strength bolts." In IABSE Symposium, Prague 2022: Challenges for Existing and Oncoming Structures. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2022. http://dx.doi.org/10.2749/prague.2022.0173.

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<p>Rivet joints are widely applied in the connections of steel bridges prior to 1950 owing to their tightness and strength. Some rivets become loosened or corroded after repeated loading and long- term usage. Previous studies indicate that replacing riveted joints with a high-strength bolt to achieve friction may be the best approach for repairing a riveted joint. However, for a long riveted joint, which has an uneven load distribution, the removal of individual rivets may overload the other rivets. This study focuses on long riveted joints at the bottom flange of an actual riveted bridge. The load redistribution mechanism involved when the rivet is removed under a dead load is investigated by performing a finite element (FE) simulation. The FE analysis results show that when a rivet is replaced by a bolt, the rivet’s load transferring ability is affected more by rivets near the bolts, whereas more distant rivets pose almost no effects.</p>
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Chen, Yu, Takashi Yamaguchi, Motoshi Yamauchi, and Keita Ueno. "Slip coefficient of 90-year-old riveted joint surface with red lead paint for corrosion." In IABSE Congress, Ghent 2021: Structural Engineering for Future Societal Needs. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2021. http://dx.doi.org/10.2749/ghent.2021.0598.

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<p>Before 1950, steel bridges were basically connected by rivets. Most of the steel bridge has been replaced due to aging or corrosion. However, many rivet bridges are still being in service; some of the rivets might be corroded and loosen due to the paint coating's deterioration. The riveted bridge has to repair by replacing the corroded rivets with high-strength bolts for friction connection. However, the slip coefficient of riveted joint surfaces with red lead treatment is not specified. In this study, specimens cut out from a 90-year-old riveted bridge's joint section and evaluated the riveted joint surface's aging condition by microscope observation and elemental analysis. The slip and pressure distribution tests are also conducted to investigate the slip coefficient and pressure distribution of riveted joints' surface. It is found that the joint surface is not flat, the average slip coefficient is 0.274, and the −2&#120590; is calculated to 0.169.</p>
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Chen, Yu, Takashi Yamaguchi, Motoshi Yamauchi, and Keita Ueno. "Slip coefficient of 90-year-old riveted joint surface with red lead paint for corrosion." In IABSE Congress, Ghent 2021: Structural Engineering for Future Societal Needs. Zurich, Switzerland: International Association for Bridge and Structural Engineering (IABSE), 2021. http://dx.doi.org/10.2749/ghent.2021.0598.

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<p>Before 1950, steel bridges were basically connected by rivets. Most of the steel bridge has been replaced due to aging or corrosion. However, many rivet bridges are still being in service; some of the rivets might be corroded and loosen due to the paint coating's deterioration. The riveted bridge has to repair by replacing the corroded rivets with high-strength bolts for friction connection. However, the slip coefficient of riveted joint surfaces with red lead treatment is not specified. In this study, specimens cut out from a 90-year-old riveted bridge's joint section and evaluated the riveted joint surface's aging condition by microscope observation and elemental analysis. The slip and pressure distribution tests are also conducted to investigate the slip coefficient and pressure distribution of riveted joints' surface. It is found that the joint surface is not flat, the average slip coefficient is 0.274, and the −2&#120590; is calculated to 0.169.</p>
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Charkasov, Shahin. "Calculation of Equal Resistance Riveted Joint." In 2nd International Scientific-Practical Conference "Machine Building and Energy: New Concepts and Technologies". Switzerland: Trans Tech Publications Ltd, 2024. http://dx.doi.org/10.4028/p-eejbe5.

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Rivet joints are used in structures that can withstand large vibration and repeated loads, as well as for connecting parts made of non-weldable materials and not allowing welding due toheating parts. In addition, riveted connections widely used to connect seversl parts in one package. In instrument making, rivet connections are used more often than in mechanical engineering. Among all constructions applied in the technique, constructions with equal resistance are considered optimal. Thus, equal stresses are created in any element of these constructions and even at any point of each element. When the value of these stresses is equal to the allowable stress, the mass of the structure is minimal. With a theoretically correct choice of the optimal elements of the connection, its destruction should occur along all of the above sections simultaneously. Riveted connections must be of equal strength. This means that the calculation must ensure the strength of the rivets against shear and crushing, the walls of the holes for the rivets-against crushing, thr parts connected along weakened sections-against tension, and their edges-against shear (puncture). The issue of design of riveted joint with equal resistance is considered. A formula has been obtained that indicates that the diameter of the rivet depends on the thickness, width and number of rivets of the connected parts (sheets).
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Ferracci, Michele, Francesco Vivio, and Vincenzo Vullo. "Structural Analysis of Riveted Structures Using a New FE Modelling Technique." In ASME 2010 10th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2010. http://dx.doi.org/10.1115/esda2010-24875.

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A theoretical approach, in order to define the structural behaviour of riveted joints, is presented. The closed form solutions lead to the definition of a Rivet Element useful to FE models of multi-riveted structures. The objective is an accurate evaluation of the local stiffness of riveted joints in FE analysis, which is fundamental to perform a reliable simulation of multi-joint structures and, consequently, a good estimate of loads acting on connections; this makes it possible to introduce new general criteria allowing, for example, to predict fatigue behaviour. On the other hand, a low number of degrees of freedom is needed when several connections are present in a complex structure. The goal is to reach a reliable model of the rivet region which can be used as the basis to develop a Rivet Element in FE analysis. The proposed Rivet Element combines the precision in the simulation with a very limited number degrees of freedom in the finite element model of a complex structure having several rivets. In the present paper the structural behavior of two simple riveted specimens is investigated experimentally and numerically using a new Rivet Element. A comparison with a joint model performed with very refined non-linear 3D models of rivet and with experimental data is performed and a good agreement is shown.
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Iyer, K., C. A. Rubin, and G. T. Hahn. "Three-Dimensional Analysis of Double Rivet-Row Lap Joints: Part II — Countersunk Rivets." In ASME 2001 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/imece2001/de-25103.

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Abstract Three-dimensional finite element analysis of an elastic, double rivet-row, aluminum alloy lap joint with countersunk, aluminum and steel rivets, is presented. Relations between the connection compliance, rivet deformation, peak contact pressures and slip amplitudes, in the absence of interference and clamp-up, are described. Analysis of a connection with non-countersunk rivets is presented in a companion paper. The trends seen in the results are similar to those obtained with non-countersunk rivets, although the peak stress concentrations in the present case are much higher. A superposition approach for estimating stress concentration factors in the panels of multi-row riveted connections with standard or countersunk rivets is presented.
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Liu, Jiemin, and Toshiyuki Sawa. "Stress Analysis and Strength Evaluation of Single-Lap Adhesive Joints Combining Rivets Subjected to External Bending Moments." In ASME 1999 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/imece1999-1186.

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Abstract Stress analysis and strength evaluation of single-lap adhesive joints combining rivets subjected to external bending moments are conducted by three-dimensional finite element analysis (FEA). In this analysis, the effects of the ratio of Young’s moduli of the rivets to that of the adherends, the initial tightening force produced in the rivets, the adhesive layers between the rivet heads and the adherends, and the positions of the rivets on the stress distributions at the interfaces between the adherends and the adhesives are examined. The rupture process of the single-lap adhesive joint combining rivets is demonstrated. The strength of single-lap adhesive joints combining rivets is evaluated by the maximum principal strain criterion using the maximum principal strain at the adhesive interfaces. The FEA results show that the failure of single-lap adhesive joints and single-lap adhesive joints combining rivets with thinner adherends are due to large elasto-plastic deformation of the adherends. For single-lap adhesive joints of thick adherends, the rupture is initiated from the edge of the adhesive interface. Experiments to measure the strength of single-lap adhesive joints, single-lap riveted joint and single-lap adhesive joints combining rivets were carried out. The failure types of single-lap adhesive joints and single-lap adhesive joints combining rivets obtained from the experiments coincide with the FEA results. The experimental results also show that the failure of single-lap riveted joints with thinner adherends is due to large plastic deformation of the adherends. However, for single-lap riveted joints with thick adherends it is shown that their failure is caused by the rupture of the rivets. Finally, it is found that fitted rivets in single-lap adhesive joints of thick adherends can enhance the joint strength.
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Notohardjono, Budy, Richard Ecker, and Shawn Canfield. "Dynamics Modeling and Analysis of Riveted Mainframe Computer Structure." In ASME 2017 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/pvp2017-65140.

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A typical mainframe computer rack is narrow, tall and long. In certain installations, during its functional operation, the server can be subjected to earthquake events. The rack is a steel structure joined together with steel rivets. One of the rack’s functions is to protect the critical components such as the processor, input-output and storage drawers from excessive motion by minimizing the amount of deflection. The riveted joints pose a challenge in accurately representing more than three thousand joints in a finite element (FE) model. In the FE model, bonding together sheet metal regions around the rivet joints will lead to a significantly stiffer model than the actual structure. On the other hand, an accurate representation of the riveted joints will lead to a better representation of the dynamic response of the server rack under vertical and horizontal loadings. This paper presents a method of analyzing rivet joints. The rivet joints are represented by beam elements with cylindrical cross-sections in the FE model. This is accomplished by identifying two parallel or overlapping plates and inserting discrete beam elements at the riveted joint. This method will be used to predict the dynamics modes of the structure. To validate the FE model, a prototype server rack was subjected to side to side vibration tests. A sine sweep vibration test identifies dominant mode shapes and the transmissibility of the input vibration. The results of the tests on the prototype rack serve as input for FE model refinement. The test data show that representing the riveted joints with beams does provide results that closely match the actual test data. A validated FE model will be used to evaluate dominant vibration modes for several configurations of rack weight as well as configurations to stiffen the structure in the side to side direction. The dynamic mode shapes visualize the effect of stiffening brackets on dominant frequencies of the rack. The optimal stiffening design will be the one that results in the minimum deflection under the standard testing profile.
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Siva Sankara Rao, Yemineni, Kutchibotla Mallikarjuna Rao, and V. V. Subba Rao. "Investigation on Fatigue Life Prediction of Riveted Cantilever Beam Using FEA Approach." In ASME 2021 40th International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/omae2021-63430.

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Abstract Different structural elements of automobiles, ships, aircraft wings and fuselages, turbines, nuclear reactors, and other machine components are susceptible to variable loading condition. Due to this type of loading situation all the mentioned structures are undergone to the formation of internal cracks, these cracks will be grown and eventually lead to the failure of the structures. Hence, the fatigue phenomenon due to variable loading conditions is a major threat and has come into address with the technological development that happening is now a days. To avoid the failure of structures due to fatigue loading condition structures are provided with different fasteners like rivets, bolts, tack welds, etc. In this study, the structures analyzed are cantilever beams, the fasteners considered are rivets, the loading considered for analysis is fully reversed cyclic loading, and the analysis considered is the fatigue analysis, the mode of analysis is a simulation using FEA software named ANSYS R19.2 WORKBENCH software. The variable parameters considered are rivet diameter, load, and coefficient of friction at the common interface of riveted specimens. Here in this analysis, the beam dimensions are kept constant. Besides, in this study, the comparison of fatigue life for solid and riveted cantilever beams of identical dimensions is presented. The material considered for the rivets and beams is aluminum alloy.
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Sawa, Toshiyuki, and Ryo Nogaito. "FEM Stress Analysis and Strength of Adhesive-Rivets Combination Joints Under Tensile Shear Loadings." In ASME 2007 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/detc2007-34455.

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Stress distributions in adhesive-rivets combination joints under tensile shear loadings are analyzed using a three-dimensional finite element method. The effects of the adherend thickness, the number of rivets and the rivet locations on the stress distributions at the interfaces are examined. Experiments to measure the rupture loads of the joints were carried out. As the results, it was found that the peel stress near the edges of the interfaces decreased as the adherend thickness increased. The maximum value of the maximum principal stresses near the edges of the interfaces decreased as the interval between the two rivets in the longitudinal direction decreased in the case where two rivets were combined. However, small effect of the interval between the two rivets in the lateral direction was found in the case of two rivets. The maximum value of the maximum principal stresses near the edges of the interfaces decreased as the interval between the four rivets in the longitudinal direction decreased and that in the lateral direction increased in the case where four rivets were combined. Discussion on the rupture loads of adhesive-rivets combination joints was made. The rupture loads of the joints increased as the number of rivets increased. The rupture loads of the adhesive-rivets combination joints could be increased more than those of only-riveted joints in the case of two rivets. The rupture loads of adhesive-rivets combination joints were found to be almost the same as those of only-riveted joints in the case of four rivets.

Reports on the topic "Riveted":

1

Bower, John E., Mark R. Kaczinski, Zouzhang Ma, Yi Zhou, John D. Wood, and Ben T. Yen. Structural Evaluation of Riveted Spillway Gates. Fort Belvoir, VA: Defense Technical Information Center, June 1994. http://dx.doi.org/10.21236/ada281492.

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Han, Li, Ken William Young, Richard Hewitt, and Andreas Chrysanthou. The Effect of Breakthrough on the Mechanical Behavior of Self-Piercing Riveted Aluminum 5754-HSLA Joints. Warrendale, PA: SAE International, May 2005. http://dx.doi.org/10.4271/2005-08-0203.

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Agudelo Urrego, Luz María, Chatuphat Savigamin, Devansh Gandhi, Ghadir Haikal, and Antonio Bobet. Assessment of Pipe Fill Heights. Purdue University Press, 2023. http://dx.doi.org/10.5703/1288284317612.

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The design of buried pipes, in terms of the allowable minimum and maximum cover heights, requires the use of both geotechnical and structural design procedures. The geotechnical procedure focuses on estimating the load on the pipe and the compressibility of the foundation soil. The focus of the structural design is choosing the correct cross-section details of the pipe under consideration. The uncertainties of the input parameters and installation procedures are significant. Because of that, the Load Resistance Factor Design (LRFD) method is considered to be suitable for the design of buried pipes. Furthermore, the interaction between the pipe structure and surrounding soil is better captured by implementing soil-structure interaction in a finite element numerical solution technique. The minimum cover height is highly dependent on the anticipated traffic load, whereas the maximum cover height is controlled by the section properties of the pipe and the installation type. The project focuses on the determination of the maximum cover heights for lock-seam CSP, HDPE, PVC, polypropylene, spiral bound steel, aluminum alloy, steel pipe lock seam and riveted, steel pipe and aluminum arch lock seam and riveted, non-reinforced concrete, ribbed and smooth wall polyethylene, smooth wall PVC, vitrified clay, structural plate steel or aluminum alloy pipe, and structural plate pipe arch steel, or aluminum alloy pipes. The calculations are done with the software CANDE, a 2D plane strain FEM code that is well-accepted for designing and analyzing buried pipes, that employs the LRFD method. Plane strain and beam elements are used for the soil and pipe, respectively, while interface elements are placed at the contact between the pipe and the surrounding soil. The Duncan-Selig model is employed for the soil, while the pipe is assumed to be elastic. Results of the numerical simulations for the maximum fill for each type and size of pipe are included in the form of tables and figures.
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Reichle, Erich Edward. Rivet Replacement Analysis. Fort Belvoir, VA: Defense Technical Information Center, December 1999. http://dx.doi.org/10.21236/ada374408.

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Wolfe, Ronald W., Marshall Begel, and Bruce Craig. Timber rivets in structural composite lumber. Madison, WI: U.S. Department of Agriculture, Forest Service, Forest Products Laboratory, 2004. http://dx.doi.org/10.2737/fpl-gtr-153.

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Begel, Marshall, Ronald W. Wolfe, and Douglas C. Stahl. Timber rivet connections in US domestic species. Madison, WI: U.S. Department of Agriculture, Forest Service, Forest Products Laboratory, 2004. http://dx.doi.org/10.2737/fpl-rp-619.

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Doi, Shigeru, and Takao Mori. Tensile Shear Strength of Aluminum-Steel Rivet Joint. Warrendale, PA: SAE International, September 2005. http://dx.doi.org/10.4271/2005-08-0540.

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Hsu, Tian-Jian, Fengyan Shi, and James T. Kirby. Interactions of Waves, Tidal Currents and Riverine Outflow and their Effects on Sediment Transport (RIVET II). Fort Belvoir, VA: Defense Technical Information Center, September 2013. http://dx.doi.org/10.21236/ada598090.

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Hsu, Tian-Jian, and Fengyan Shi. Interactions of Waves and River Plume and their Effects on Sediment Transport at River Mouth (RIVET I). Fort Belvoir, VA: Defense Technical Information Center, September 2013. http://dx.doi.org/10.21236/ada598089.

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Donlon, Francis P., and Brian A. Levine. 120-mm Target Practice Cone Stabilized Discarding Sabot with Tracer (TPCSDS-T) M865 (E3) Rework Report (Pop-Rivet Design). Fort Belvoir, VA: Defense Technical Information Center, October 2002. http://dx.doi.org/10.21236/ada411174.

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