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Relevant bibliographies by topics / Lap joints

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Academic literature on the topic 'Lap joints'

Author: Grafiati

Published: 4 June 2021

Last updated: 4 February 2022

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Journal articles on the topic "Lap joints"

1

Khalid, Asad A. "Effect of Interface Geometry on Strength of Single Lap Adhesive Joint of Sisal-Glass/Epoxy Laminates." Key Engineering Materials 858 (August 2020): 20–26. http://dx.doi.org/10.4028/www.scientific.net/kem.858.20.

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In this project, experimental work on tensile behaviour of single lap adhesive joints of sisal, glass and hybrid sisal-glass/epoxy composite laminates has been carried out. Composite laminates were fabricated by hand lay-up method using chopped strand mat sisal and glass fibers with epoxy resin matrix. Lab joints of four interface geometries; straight flat, triangular, rectangular and sinusoidal were fabricated. Tensile load-displacement relations were drawn and discussed. Effect of interface geometry and material type on maximum load and strength of the single lap joint was investigated. Failure mechanism of the fractured specimens was discussed. Results show that the glass/epoxy lap joints with semi-circular adhesive interface geometry supported load higher respectively 14.26%, 26.13%, and 30.79% than rectangular, triangular and straight flat interface geometries. Glass/epoxy lap joint with semi-circular interface geometry supported tensile load higher 5.61% and 21.83% than that obtained from hybrid sisal-glass and sisal/ epoxy adhesive joints. While the shear strength was found higher respectively 6.19% and 18.69%. Adhesive failure mode was observed for most of the single lap joints investigated. Mixed failure mode of adhesive and adherend materials was observed on the sisal/epoxy lap joints.

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2

Sadowski, T., and P. Golewski. "Numerical Study of the Prestressed Connectors and Their Distribution on the Strength of a Single Lap, a Double Lap and Hybrid Joints Subjected to Uniaxial Tensile Test." Archives of Metallurgy and Materials 58, no. 2 (June 1, 2013): 579–85. http://dx.doi.org/10.2478/amm-2013-0041.

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Prestressed joints are widely used in construction using connectors in the form of screws, whose task is to strong clamping of joined parts, thereby the internal forces in joint are transferred by surface friction contact of the elements. In the automotive and aerospace industries hybrid joints are more widely applied. Mechanical connectors are added to the adhesive joint in form of rivets, screws or clinch increasing its strength properties. The aim of this study was to determine how the prestressed connectors influence the mechanical response of hybrid, single and double lap joints. The influence of different distribution of the connectors was also investigated. Numerical study was conducted in ABAQUS program. Mechanical connectors were modeled by using fasteners, that allowed for a considerable simplification of the numerical model. In their application, there is no need for an additional submodels for connectors in the form of the rivet or the bolt. Prestressing is activated by direct application of the force to the connector. In the numerical examples the authors assumed that the diameter of the mechanical connectors was equal to 6mm and shear strength was equal 1kN. Adhesive layers were modeled by using cohesive elements for which maximum shear stresses and fracture energy were specified. The layer thickness was assumed to be equal 0.1mm and it was initially removed from the areas where mechanical connectors were placed. Two types of joints were analysed in the study: the single lap joint with lap dimensions 40x40mm as well as the double lap joint with lap dimensions 40x20mm, from which it results that theoretical strength of both connections should be the same. The prestressing of connectors was introduced by the force 1.5kN. For all pure - mechanical joints and for single lap joints positive effects were obtained. For double lap joints additional prestressing did not significantly affect for their strength. The influence of distribution of mechanical connectors was additionally analyzed by consideration of three configurations, where the rows of rivets were located at distances of 5, 10 and 15mm from the lap edge. The maximum increase of the load capacity by 24% was achieved for single lap joint as well as 35.7% for double lap joint. The obtained numerical results indicate the positive effects of additional pressure and allows for practical suggestions how to correct and optimize spacing distance of mechanical connectors in hybrid joints to get better mechanical response.

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3

Lam, Angus C. C., J. J. Roger Cheng, Michael C. H. Yam, and Gaylene D. Kennedy. "Repair of steel structures by bonded carbon fibre reinforced polymer patching: experimental and numerical study of carbon fibre reinforced polymer – steel double-lap joints under tensile loading." Canadian Journal of Civil Engineering 34, no. 12 (December 2007): 1542–53. http://dx.doi.org/10.1139/l07-074.

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The behavior of carbon fibre reinforced polymer (CFRP) composite bonded to a steel plate double-lap joint was investigated experimentally. A total of 19 specimens were tested with the major test parameters being the bonded lap length, LL, and the axial adherend stiffness ratio, ETR. Five of the 19 specimens were prepared using CFRP sheets, and the rest using CFRP plates. Two CFRP plate specimens were prepared with a tapered lap joint, and their results were compared with those of counterpart specimens prepared without tapered lap joints. In general, the behavior of specimens made from either CFRP sheets or CFRP plates were similar. The joint's axial load carrying capacity increased with increasing LL up to a certain limit, when the joint's load carrying capacity could no longer be increased by increasing LL. However, experimental results showed that a larger failure deformation could be achieved by increasing LL past this limit. Specimens that had the same inner adherend thickness but higher axial adherend stiffness ratios showed higher axial load carrying capacities. Test results also showed that the strengths of tapered lap joints were almost the same as those of nontapered lap joints with the same LL. Nonlinear finite element analysis was carried out to study the stress–strain behavior of the adherend and the adhesive of the double-lap joint. Using finite element analysis results in an analytical solution obtained from the literature, predictions of the joint's maximum axial strength and minimum required LL were made. This analytical solution provided good predictions when compared with test results, producing test to predicted ratios from 0.88 to 1.14.

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4

Fongsamootr, Thongchai, Charoenyut Dechwayukul, Notsanop Kamnerdtong, Carol A. Rubin, and George T. Hahn. "Parametric Study of Combined Adhesive-Riveted Lap Joints." Key Engineering Materials 261-263 (April 2004): 399–404. http://dx.doi.org/10.4028/www.scientific.net/kem.261-263.399.

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Riveted lap joints are widely used to assemble complex structures, e.g. aircraft fuselages. A thin layer of adhesive (sealant), is normally applied to lap joints in order to restrict the entry of moisture and retard corrosion. In this work, combined adhesive-riveted lap joints were studied to understand the effect of three parameters: panel thickness, adhesive stiffness and adhesive layer thickness, on single row non-countersunk riveted lap joints. Finite element analysis (FEA), along with Thin Adhesive Layer Analysis (TALA-developed for simulating the adhesive layer in lap joint models), were used to analyze the joint behavior. In previous studies, the stress concentration factor for single row riveted lap joints was found to be approximately 6.1, and the stress concentration factor for sealed riveted lap joints was approximately 5.2 for a 180 micron thick sealant layer. In this study, panel thickness, adhesive stiffness and adhesive layer thickness were varied parametrically in FEA analyses to determine their affects on the joints. The FEA/TALA results were used to predict the fatigue life of the joints as functions of the three parameters. The results show that the maximum tensile stress is smaller with a smaller panel thickness. The results also showed that the stress concentration factor in the joints was reduced when the stiffness of the adhesive layer was increased or when the thickness of the adhesive layer was decreased. Finally, fatigue tests showed that the fatigue life of the combined adhesive-riveted lap joints was greater than for riveted lap joints without adhesive.

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Sanati, M., Y. Alammari, J. H. Ko, and S. S. Park. "Identification of joint dynamics in lap joints." Archive of Applied Mechanics 87, no. 1 (September 21, 2016): 99–113. http://dx.doi.org/10.1007/s00419-016-1179-8.

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Vaziri, A., H. Nayeb-Hashemi, and H. R. Hamidzadeh. "Experimental and Analytical Investigations of the Dynamic Response of Adhesively Bonded Single Lap Joints." Journal of Vibration and Acoustics 126, no. 1 (January 1, 2004): 84–91. http://dx.doi.org/10.1115/1.1596550.

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Dynamic response of single lap joints, subjected to a harmonic peeling load is studied theoretically and experimentally. In the theoretical part, dynamic response of a single lap joint clamped at one end and subjected to a harmonic peeling load at the other end is investigated. Adherents are modeled as Euler-Bernouli beams joined in the lap area by a viscoelastic adhesive layer. Both axial and transverse deformations of adherents are considered in deriving the equations of motion. The effects of adhesive layer thickness, mechanical properties and its loss factor on the dynamic response of the joint are investigated. Furthermore, effects of defects such as a void in the lap area on the dynamic response of the joints are studied. The results showed that frequencies where peak amplitudes occurred were little dependent on the adhesive loss factor. However, peak amplitudes reduced for joints with a higher adhesive loss factor. Furthermore, the results indicated that for the joint geometries and properties investigated the system resonant frequencies were not affected by the presence of a central void covering up to 80% of the overlap length. In the experimental part, single lap joints were fabricated using 6061-T6 Aluminum. Adherents were joined together using Hysol EA 9689 adhesive film. Joints with various central voids were manufactured by removing adhesive film from the desired area of lap joints prior to bonding adherents. Dynamic responses of the joints were investigated using the hammer test technique. The system response was measured using both an accelerometer and a noncontact laser vibrometer. The natural frequencies of the joints obtained by using the laser vibrometer were very close to those obtained theoretically. However, natural frequencies obtained by using an accelerometer depended on the accelerometer location in the system, which was attributed to its mass contribution to the over- all system mass. A central void covering less than 80% of the overlap length had little effect on the system resonance frequencies. This was in agreement with the theoretical results. In contrast total system-damping ratios were a function of the void size. Joints without a void exhibited higher damping.

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Razavi, SMJ, MR Ayatollahi, M. Samari, and LFM da Silva. "Effect of interface non-flatness on the fatigue behavior of adhesively bonded single lap joints." Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications 233, no. 7 (November 6, 2017): 1277–86. http://dx.doi.org/10.1177/1464420717739551.

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This paper addresses numerical and experimental examination of the role of zigzag interface shapes on the load bearing capacity and fatigue life of adhesively bonded single lap joints. Aluminum adherends with non-flat zigzag interfaces were tested under both quasi-static and fatigue loading conditions. The quasi-static test results revealed that the non-flat adhesive joints have higher load bearing capacity compared to the conventional flat single lap joints. Comparative fatigue tests with different loading levels revealed that the non-flat zigzag single lap joint had considerably higher fatigue life than the conventional lap joint.

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He, Changshu, Zhiqiang Zhang, Ying Li, Jingxun Wei, Menggang Zhai, Su Zhao, and Xiang Zhao. "Interface Characteristics and Mechanical Properties of Ultrasonic-Assisted Friction Stir Lap Welded 7075-T6 Aluminium Alloy." Materials 13, no. 23 (November 25, 2020): 5335. http://dx.doi.org/10.3390/ma13235335.

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In this work, friction stir lap welding (FSLW) and ultrasonic-assisted friction stir lap welding (UAFSLW) was applied to 6-mm-thick 7075-T6 alloy sheets using three welding tools with the same process parameters. The joint formation, microstructural characteristics, and mechanical properties of the resulting lap joints were then investigated. The results showed that ultrasonic vibration significantly promoted the flow of metal at the interface, enlarged the size of the stirred zone (SZ), and reduced the angle between the hook defect and the interface. During lap shear testing, the FSLW and UAFSLW joints fractured in a similar manner. The fracture modes included tensile fracture, shear fracture, and a mixture of both. Cold lap and hook defects may have served as crack-initiation zones within the joint. Under configuration A (i.e., upper sheet on the retreating side (RS)), all joints failed in the shear-fracture mode. The effective lap width (ELW) of the joint welded using tool T2 was the greatest. This resulted in a higher shear fracture strength. The maximum shear fracture strength of the UAFSLW joint was 663.1 N/mm. Under configuration B (i.e., upper sheet on the advancing side (AS)), the shear fracture strength was greatly affected by the fracture mode. The highest shear fracture strength of the UAFSLW joint, 543.7 N/mm, was welded by tool T3. Thus, under otherwise identical conditions, UAFSLW joints can withstand a greater fracture shear strength than FSLW joints, as ultrasonic vibration helps to mix the material at the interface, thus, enlarging the SZ and diminishing the cold lap defects.

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Witek, Lucjan. "INFLUENCE OF PLASTIC DEFORMATION OF ADHEREND MATERIAL ON STRESS DISTRIBUTION IN ADHESIVE LAP JOINTS." Acta Metallurgica Slovaca 23, no. 4 (December 4, 2017): 304. http://dx.doi.org/10.12776/ams.v23i4.1010.

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<p class="AMSmaintext">In the engineering analysis of adhesive lap joints the linear-elastic model of adherend material is often used. In some cases, when the joined material has a low yield stress, this assumption causes errors in stress estimation in the adhesive layer or adherend. In this study the results of numerical stress and strain analysis of single lap adhesive joints were presented. In performed analysis both the linear-elastic and the elastic-plastic models of adherend materials were considered. In the first part of the work the mechanical properties of joined material were obtained using the experimental investigations. In the next part of the work the discrete model of joint was created. The results of nonlinear finite element analysis showed that in the case of joining of materials with low yield stress the plastic deformation in adherend occurs at load much smaller than destructive force of the joint. In this kind of joints the plastic deformation of adherend influences a rapid stress increase in the adhesive layer, at the final stage of loading. This phenomenon causes a decrease of strength of single lap adhesive joints of elastic-plastic materials.</p>

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Takashima, Yasuhito, Tomo Washio, and Fumiyoshi Minami. "Evaluation of Tensile Shear Strength for Lap Joint of Dissimilar Steels." Materials Science Forum 1016 (January 2021): 1454–59. http://dx.doi.org/10.4028/www.scientific.net/msf.1016.1454.

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The influence of different thickness combinations was investigated on the strength of the lap joint of dissimilar steels. In this study, lap joints of dissimilar steels were welded by laser welding. The tensile shear test was conducted for the lap joints. Rotational deformation process around the weld bead of the lap joint was observed by a digital video camera during the test. Motion analysis from the video of the tensile shear test indicated that the rotation angle around the weld bead was reduced by overlapping higher strength grade steel. Three-dimensional elastic-plastic finite element analysis was performed for the tensile shear test of the lap joint. The numerically calculated deformation behavior of the lap joint subjected to tensile shear loading showed reasonable agreement with the experimental record. It was found that the rotation angle was reduced and tensile shear strength of the lap joint increase by overlapping higher strength grade steel sheet.

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Dissertations / Theses on the topic "Lap joints"

1

Ekh, Johan. "Multi-fastener single-lap joints in composite structures." Doctoral thesis, Stockholm : Royal Institute of Technology, 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-4006.

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Chazerain, Aurélie. "Characterization of resistance-welded thermoplastic composite double-lap joints." Thesis, McGill University, 2009. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=67019.

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An investigation of resistance welding of thermoplastic composite double-lap shear joints is presented. Double-lap shear specimens consisting of carbon fibre/poly-etherether-ketone (PEEK/CF), carbon fibre/poly-etherketone-ketone (PEKK/CF), carbon fibre/poly-ether-imide (PEI/CF) and glassfibre/poly-ether-imide (PEI/GF) were resistance-welded using a stainless steel mesh heating element. The objective of this work was to study the mechanical performances of the double lap shear resistance-welded joints and to compare them with the single lap shear resistance-welded joints. The welded specimens were analyzed using static and dynamic lap shear tests and optical and scanning electron microscopy. Lap shear strengths of 53 MPa, 49 MPa, 45 MPa and an extrapolated value of 34 MPa were obtained for PEEK/CF, PEKK/CF, PEI/CF and PEI/GF double-lap joints, respectively. Infinite fatigue lives were obtained at 30% for PEEK/CF and PEKK/CF, 25% for PEI/CF and 20% for PEI/GF. Resistance-welded double-lap joints were found to have equivalent static and fatigue mechanical properties compared with single-lap joints, for all materials tested.
Ce travail présente une étude des joints à recouvrement double de matériaux composites à matrice thermoplastique assemblés par soudage par résistance. Des échantillons de joints à recouvrement double constitués de fibre de carbone/polyéther éther cétone (PEEK/CF), fibre de carbone/polyéther cétone cétone (PEKK/CF), fibre de carbone/polyéther imide (PEI/CF) et fibre de verre/polyéther imide (PEI/CF), ont été assemblés pas soudage par résistance à l'aide d'un élément chauffant en acier inoxydable. L'objectif de ce travail est d'étudier les performances mécaniques des joints à recouvrement double soudés pas résistance et de les comparer avec celles des joints à recouvrement simple. Les échantillons soudés ont été analysés à l'aide de tests de chargement statiques et dynamiques, ainsi que pas microscopie optique et par microscopie électronique à balayage. Une résistance au cisaillement de 53 MPa, 49 MPa, 45M Pa, et une valeur extrapolée de 34 MPa ont été obtenues pour les joints à recouvrement double de PEEK/CF, PEKK/CF, PEI/CF et PEI/GF, respectivement. Une durée de vie indéterminée en fatigue de 30% du chargement statique pour les joints de PEEK/CF et PEKK/CF, de 25% pour les joints de PEI/CF, et de 20% pour les joints de PEI/GF ont été obtenues. Pour chacun des matériaux testés, les joints à recouvrement double soudés par résistance ont donné lieu à des propriétés mécaniques en statique et en fatigue équivalentes à celles des joints à recouvrement simple.

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3

Doering, Kenneth Thomas Nathaniel. "Fatigue of friction stir welded lap joints with sealants." Diss., Rolla, Mo. : Missouri University of Science and Technology, 2009. http://scholarsmine.mst.edu/thesis/pdf/Doering_09007dcc80627994.pdf.

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Thesis (M.S.)--Missouri University of Science and Technology, 2009.
Vita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed April 9, 2009) Includes bibliographical references (p. 118-127).

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Dinsley, Christopher Paul. "Fatigue properties of dissimilar metal laser welded lap joints." Thesis, Sheffield Hallam University, 2004. http://shura.shu.ac.uk/19561/.

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This work involves laser welding austenitic and duplex stainless steel to zinc-coated mild steel, more specifically 1.2mm V1437, which is a Volvo Truck Coiporation rephosphorised mild steel. The work investigates both tensile and lap shear properties of similar and dissimilar metal laser welded butt and lap joints, with the majority of the investigation concentrating on the fatigue properties of dissimilar metal laser welded lap joints. The problems encountered when laser welding zinc-coated steel are addressed and overcome with regard to dissimilar metal lap joints with stainless steel. The result being the production of a set of guidelines for laser welding stainless steel to zinc-coated mild steel. The stages of laser welded lap joint fatigue life are defined and the factors affecting dissimilar metal laser welded lap joint fatigue properties are analysed and determined; the findings suggesting that dissimilar metal lap joint fatigue properties are primarily controlled by the local stress at the internal lap face and the early crack growth rate of the material at the internal lap face. The lap joint rotation, in turn, is controlled by sheet thickness, weld width and interfacial gap. Laser welded lap joint fatigue properties are found to be independent of base material properties, allowing dissimilar metal lap joints to be produced without fatigue failure occurring preferentially in the weaker parent material, irrespective of large base material property differences. The effects of Marangoni flow on the compositions of the laser weld beads are experimentally characterised. The results providing definite proof of the stirring mechanism within the weld pool through the use of speeds maps for chromium and nickel. Keywords: Laser welding, dissimilar metal, Zinc-coated mild steel, Austenitic stainless steel, Duplex stainless steel, Fatigue, Lap joint rotation, Automotive.

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Curnutt, Austin. "Research on the mechanics of CFRP composite lap joints." Thesis, Kansas State University, 2017. http://hdl.handle.net/2097/38191.

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Master of Science
Department of Architectural Engineering
Donald J. Phillippi
For this thesis, research was performed on CFRP bonded composite lap-joints with one and two continuous laminas through the lap. Composite wraps used to retrofit existing structures use lap joints to maintain their integrity. The use of composites for retrofitting structures has many advantages over traditional methods, such as steel jacketing, and is becoming more widely accepted in the structural engineering industry. While much literature exists documenting the performance of composite wraps as a whole when applied to concrete columns, less information is available on the behavior of the lap-joint of the wrap. Developing a better understanding of how the lap-joint behaves will help researchers further understand composite column wraps. This research sought to determine what affect continuous middle laminas may have on the stiffness of lap joints and whether or not stress concentrations exist in the lap-joint due to a change in stiffness.

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6

Scott, Jason P. "Corrosion and multiple site damage in riveted fuselage lap joints." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq22127.pdf.

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7

Li, Gang. "Deformation of balanced and unbalanced adhesively bonded single-lap joints." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape4/PQDD_0030/NQ65464.pdf.

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Scott, Jason P. (Jason Philip) Carleton University Dissertation Engineering Mechanical and Aerospace. "Corrosion and multiple site damage in riveted fuselage lap joints." Ottawa, 1997.

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9

Karachalios, E. F. "Stress and failure analysis of adhesively bonded single lap joints." Thesis, University of Bristol, 1999. http://hdl.handle.net/1983/72fde066-0a88-4b2b-83ea-c2c08f0ce0fc.

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10

Coates, Cameron Wayne. "New concepts for strength enhancement of co-cured composite single lap joints." Diss., Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/12937.

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Books on the topic "Lap joints"

1

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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2

Lameris, J. The static strength of mechanically fastened carbon-epoxy joints without bending. Amsterdam, Netherlands: National Aerospace Laboratory, 1989.

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3

Skorupa, Andrzej. Riveted Lap Joints in Aircraft Fuselage: Design, Analysis and Properties. Dordrecht: Springer Netherlands, 2012.

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4

Fung, Chin-Ping. An experimental and numerical study of riveted single lap joints. Manchester: University of Manchester, 1994.

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5

Apalak, Mustafa Kemal. Analysis and design of adhesively bonded lap and corner joints. Birmingham: University of Birmingham, 1994.

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Skorupa, Małgorzata. Load transmission and secondary bending in lap joints of aircraft fuselage. Warsaw: Institute of Aviation Scientific Publications, 2010.

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7

Miller, M. D. The effect of non-standard spacing on simple timber lap joints. London: North East London Polytechnic, 1985.

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8

Piascik, Robert S. The characteristics of fatigue damage in the fuselage riveted lap splice joint. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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Skorupa, Andrzej. Effect of production and design related factors on the fatigue behaviour of riveted lap joints in aircraft fuselage. Warsaw: Institute of Aviation Scientific Publications, 2010.

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Pérez, Emilio Pérez. Las cotitularidades sobre bienes inmuebles. Barcelona: Bosch, 2006.

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Book chapters on the topic "Lap joints"

1

Aldanondo, Egoitz, Ekaitz Arruti, Jorge Garagorri, and Alberto Echeverria. "Dissimilar Aluminum-Steel FSW Lap Joints." In Friction Stir Welding and Processing VIII, 137–43. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2015. http://dx.doi.org/10.1002/9781119093343.ch15.

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Aldanondo, Egoitz, Ekaitz Arruti, Jorge Garagorri, and Alberto Echeverria. "Dissimilar Aluminum-Steel FSW Lap Joints." In Friction Stir Welding and Processing VIII, 137–43. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-48173-9_15.

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Fratini, L. "FSW of Lap and T-Joints." In Structural Connections for Lightweight Metallic Structures, 125–49. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/8611_2010_48.

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da Silva, Lucas F. M., Marcelo Costa, Guilherme Viana, and Raul D. S. G. Campilho. "Analytical Modelling for the Single-Lap Joint." In Strength Prediction of Adhesively-Bonded Joints, 8–46. Boca Raton, FL : Taylor & Francis Group, CRC Press, [2016] | “A science publishers book.”: CRC Press, 2017. http://dx.doi.org/10.1201/9781315370835-2.

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Mal, Ajit K., Shyh-Shiuh Lih, and Dawei Guo. "Ultrasonic Characterization of Defects in Lap Joints." In Review of Progress in Quantitative Nondestructive Evaluation, 2059–64. Boston, MA: Springer US, 1995. http://dx.doi.org/10.1007/978-1-4615-1987-4_263.

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Gresnigt, A. M., and C. M. Steenhuis. "Stiffness of Lap Joints with Preloaded Bolts." In The Paramount Role of Joints into the Reliable Response of Structures, 435–48. Dordrecht: Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-010-0950-8_38.

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Degen, Cassandra M., Lidvin Kjerengtroen, Eirik Valseth, and Joseph R. Newkirk. "Impact and Lap Shear Properties of Ultrasonically Spot Welded Composite Lap Joints." In Joining Technologies for Composites and Dissimilar Materials, Volume 10, 59–69. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-42426-2_7.

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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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Skorupa, Andrzej, and Małgorzata Skorupa. "Load Transfer in Lap Joints with Mechanical Fasteners." In Solid Mechanics and Its Applications, 115–44. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-4282-6_5.

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Wang, C. H., and L. R. F. Rose. "Stress Analysis and Failure Assessment of Lap Joints." In Recent Advances in Structural Joints and Repairs for Composite Materials, 1–26. Dordrecht: Springer Netherlands, 2003. http://dx.doi.org/10.1007/978-94-017-0329-1_1.

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Conference papers on the topic "Lap joints"

1

Birch, R. S., and M. Alves. "Dynamic Failure of Lap Joints." In SAE Brasil 97 VI International Mobility Technology Conference and Exhibit. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1997. http://dx.doi.org/10.4271/973048.

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Carpenter, William C. "Comparison of numerous lap joint theories for adhesively bonded joints." In SPIE's 1993 International Symposium on Optics, Imaging, and Instrumentation, edited by Eric A. Norland and Kenneth M. Liechti. SPIE, 1993. http://dx.doi.org/10.1117/12.158608.

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3

Whitney, James. "Stress analysis of cylindrical composite lap joints." In 39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-1884.

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4

Bellinger, N. C., R. W. Gould, and J. P. Komorowski. "Repair Issues for Corroded Fuselage Lap Joints." In World Aviation Congress & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1999. http://dx.doi.org/10.4271/1999-01-5529.

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5

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

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6

Albright, Charles E., Chris Hsu, and R. Olan Lund. "Fatigue strength of laser-welded lap joints." In ICALEO® ‘90: Proceedings of the Laser Materials Processing Conference. Laser Institute of America, 1990. http://dx.doi.org/10.2351/1.5058377.

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7

KAISER, ISAIAH, and K. T. TAN. "Gecko Inspired Adhesive Patterned Single-Lap Joints." In American Society for Composites 2020. Lancaster, PA: DEStech Publications, Inc., 2020. http://dx.doi.org/10.12783/asc35/34964.

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Bates, P. J., D. Couzens, and J. Mah. "Shear Strength of Vibration Welded Lap Joints." In SAE 2004 World Congress & Exhibition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2004. http://dx.doi.org/10.4271/2004-01-0734.

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Bellinger, Nicholas, Jerzy Komorowski, and Ronald Gould. "Corrosion Pillowing in Aircraft Fuselage Lap Joints." In 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-2023.

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Bambei, Jr., John H., and Dennis A. Dechant. "Welded Steel Pipe Lap Joints—An Evolution." In Pipelines Specialty Conference 2009. Reston, VA: American Society of Civil Engineers, 2009. http://dx.doi.org/10.1061/41069(360)111.

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Reports on the topic "Lap joints"

1

SEGALMAN, DANIEL J. A Four-Parameter Iwan Model for Lap-Type Joints. Office of Scientific and Technical Information (OSTI), November 2002. http://dx.doi.org/10.2172/805877.

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2

HEINSTEIN, MARTIN W., and DANIEL J. SEGALMAN. Bending Effects in the Frictional Energy Dissipation in Lap Joints. Office of Scientific and Technical Information (OSTI), January 2002. http://dx.doi.org/10.2172/793221.

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3

Metzinger, K. E., and T. R. Guess. How geometric details can affect the strength of adhesive lap joints. Office of Scientific and Technical Information (OSTI), December 1996. http://dx.doi.org/10.2172/425260.

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4

Koch, Gerhardus H., Le Yu, and Noriko Katsube. Mathematical Model to Predict Fatigue Crack Initiation in Corroded Lap Joints, Draft. Fort Belvoir, VA: Defense Technical Information Center, August 1998. http://dx.doi.org/10.21236/ada362602.

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5

Seto, Atsushi, Yuichi Yoshida, and Andre Galtier. Fatigue Properties of Arc-Welded Lap Joints With Weld Start and End Points. Warrendale, PA: SAE International, May 2005. http://dx.doi.org/10.4271/2005-08-0128.

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6

Gent, A. N., and C. W. Lin. Comparison of Peel and Lap Shear Bond Strengths for Elastic Joints with and without Residual Stresses. Fort Belvoir, VA: Defense Technical Information Center, May 1989. http://dx.doi.org/10.21236/ada208102.

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7

Jensen, Robert, Daniel DeSchepper, David Flanagan, Gerard Chaney, and Charles Pergantis. Adhesives: Test Method, Group Assignment, and Categorization Guide for High-Loading-Rate Applications Preparation and Testing of Single Lap Joints (Ver. 2.2, Unlimited). Fort Belvoir, VA: Defense Technical Information Center, April 2016. http://dx.doi.org/10.21236/ad1008131.

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8

GREGORY, DANNY LYNN, BRIAN R. RESOR, RONALD G. COLEMAN, and DAVID ORA SMALLWOOD. Experimental Investigations of an Inclined Lap-Type Bolted Joint. Office of Scientific and Technical Information (OSTI), April 2003. http://dx.doi.org/10.2172/810683.

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9

Mayes, Randall Lee. A feasibility study for experimentally determining dynamic force distribution in a lap joint. Office of Scientific and Technical Information (OSTI), November 2013. http://dx.doi.org/10.2172/1115248.

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Hunt, John F., and Jerrold E. Winandy. Lam I-joists : a new structural building product from small-diameter, fire-prone timber. Madison, WI: U.S. Department of Agriculture, Forest Service, Forest Products Laboratory, 2003. http://dx.doi.org/10.2737/fpl-rn-291.

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