Relevant bibliographies by topics / Stress distribution around a circular hole

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

Academic literature on the topic 'Stress distribution around a circular hole'

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Published: 3 June 2025
Last updated: 31 July 2025

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Journal articles on the topic "Stress distribution around a circular hole"

1

Jafari, Mohammad, and Mohammad Jafari. "Effect of hole geometry on the thermal stress analysis of perforated composite plate under uniform heat flux." Journal of Composite Materials 53, no. 8 (2018): 1079–95. http://dx.doi.org/10.1177/0021998318795279.

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The presence of holes in composite plates subjected to a uniform heat flux induces thermal stresses. Hole geometry is one of the important parameters in the stress distribution in perforated composite plates. In this study, using the two-dimensional thermoelastic theory, and on the basis of the Lekhnitskii' complex variable technique in steady-state condition, stress distribution around holes with different shapes in an infinite composite plate under uniform heat flux is investigated. Using a conformal mapping function, the thermal stress analysis of an infinite plate with a circular hole unde
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Kumar, R. Ramesh, S. Jose, and G. Venkateswara Rao. "Analytical Solution for W-N Criteria for the Prediction of Notched Strength of an Orthotropic Shell." Journal of Applied Mechanics 68, no. 2 (2000): 344–46. http://dx.doi.org/10.1115/1.1320452.

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Analytical solution for the tangential stress distribution ahead of a hole is needed for the theoretical prediction of notched strength of brittle laminate using the well-known W-N criteria. In the present study, tangential stress distribution in an orthotropic circular cylindrical shell under uniaxial loading with a circular hole is obtained intuitively with the use of a stress function. A good agreement is obtained for the stresses around and ahead of the circular hole in 0deg4±30degs and 90 deg laminates with the finite element results.
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Mohan, Pradeep, and R. Ramesh Kumar. "A Non-Singular Analytical Technique for Reinforced Non-Circular Holes in Orthotropic Laminate." International Journal of Applied Mechanics and Engineering 25, no. 1 (2020): 92–105. http://dx.doi.org/10.2478/ijame-2020-0007.

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AbstractThe intricacy in Lekhnitskii’s available single power series solution for stress distribution around hole edge for both circular and noncircular holes represented by a hole shape parameter ε is decoupled by introducing a new technique. Unknown coefficients in the power series in ε are solved by an iterative technique. Full field stress distribution is obtained by following an available method on Fourier solution. The present analytical solution for reinforced square hole in an orthotropic infinite plate is derived by completely eliminating stress singularity that depends on the concept
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Hidayat, Syarif, Bambang K. Hadi, Hendri Syamsudin, and Sandro Mihradi. "Stress-Distribution around Pin-Loaded Hole for Orthotropic Laminates." Applied Mechanics and Materials 842 (June 2016): 53–60. http://dx.doi.org/10.4028/www.scientific.net/amm.842.53.

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Stresses were calculated for orthotropic laminate plate loaded by a frictionless pin in a circular hole of the same diameter. These calculations were based on finite-element analysis for five laminates; 00, [±450]s, [00/900]s,[00/±450]s, and quasi-isotropic [00/±450/900]s. stress distribution, based on nominal bearing stress, were determined for wide ranges of the ratios of width to diameter and edge distance to diameter. Orthotropic had a significant influence on both the magnitude and location of the maximum tensile stress concentration on the boundary of the hole. The laminates with 00 plie
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Pazand, Kamran, and Younes Alizadeh. "Apply Artificial Neural Networks to Estimate Stress Distribution around Holes Edge in Composites." Advanced Materials Research 490-495 (March 2012): 3105–8. http://dx.doi.org/10.4028/www.scientific.net/amr.490-495.3105.

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The purpose of this paper is to estimate the fast determination of stress distribution around a circular hole in symmetric composite laminates under in-plane loading. For this purpose calculation of stress values in the composite plate around edge holes in different plies position for a finite number of input data sets using the Lekhnitskii expressions and code program. The resulting data would then be used to train artificial neural networks (ANN) which would be able to predict –accurately enough- those quantities throughout the composite plate body for any given input value in any position p
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6

Lee, Eung J., and Eric C. Klang. "Stress Distribution in an Edge-Stiffened Semi-infinite Elastic Plate Containing a Circular Hole." Journal of Applied Mechanics 59, no. 4 (1992): 789–95. http://dx.doi.org/10.1115/1.2894044.

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An edge-stiffened semi-infinite elastic plate containing a circular hole under tension at infinity has been studied using a conformal mapping technique. Melan ’s stiffener condition in Cartesian coordinates has been newly formulated as a resultant shear stress condition in bipolar coordinates. The solution is sought in series form, and by truncating the system of equations, it is numerically solved. Pertinent stress distributions are examined to illustrate the roll of the stiffener under the presence of a circular hole near the straight edge. It has been concluded that the stiffener contribute
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Mazin, V. A., V. L. Mikhaylova, and L. G. Sukhomlinov. "Transverse compression of a two-layered elastic plane with a circular hole on the border between layers." Izvestiya MGTU MAMI 9, no. 4-4 (2015): 106–10. http://dx.doi.org/10.17816/2074-0530-67079.

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The results are presented on the stress distribution in a transversally compressed two-layered elastic plane with a circular hole on the border between layers, received by using a variational fi- nite-difference procedure for solving plane elastic problems for the holed rectangular domains. The effects of the layers' elastic constants on the level of stresses around the hole are examined.
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Zhang, Shu, and Lei Meng. "Single Crystal Alloy on the Creep Behavior of Holes in Three-Dimensional Finite Element Simulation." Advanced Materials Research 462 (February 2012): 61–64. http://dx.doi.org/10.4028/www.scientific.net/amr.462.61.

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Based on finite element Method a dynamic mathematical model is established, and the simulation of stress distribution around the defects of single crystal nickel-based superalloysis also established with ANSYS. Results show that the creep lifetimes and plasticity of the single crystal nickel based superalloys are obviously decreased by microstructure defects. During high temperature creep, the stress isoline near the holes region displays the feature of the acetabuliform distribution, and possesses the bigger stress value at 45 angle direction relative to the applied stress axis. That results
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Glazov, A. L., N. F. Morozov, and K. L. Muratikov. "Laser photoacoustic evaluaion of residual stresses in metal plates with a hole." Доклады Академии наук 484, no. 3 (2019): 277–80. http://dx.doi.org/10.31857/s0869-56524843277-280.

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The nature of the change in the photoacoustic signal around the hole in samples of duralumin is studied. A com- parison of the experimental results with the solution of the classical problem for stress distribution around a circular hole in a prestressed plate is made. A good correspondence between the behavior of the photoacoustic signal with piezoelectric recording and the distribution of stresses around the hole is demonstrated. The possibility of estimating the internal stresses by the photoacoustic method in combination with the hole drilling method is shown.
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Глазов, А. Л., та К. Л. Муратиков. "Диагностика остаточных напряжений в биметаллических пластинах алюминий-сталь с использованием лазерного ультразвука и зондирующего отверстия". Журнал технической физики 46, № 23 (2020): 33. http://dx.doi.org/10.21883/pjtf.2020.23.50346.18435.

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The character of changes in laser photoacoustic signals near small-diameter holes in layers of aluminum and steel in a bimetallic plate obtained by hot rolling is investigated. The experimental results are compared with the solution of the classical Kirsch problem for stress distribution around a circular hole in a prestressed material. The possibility of assessing internal stresses by a laser photoacoustics in combination with the hole drilling method in industrial bimetallic plates is shown.
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Dissertations / Theses on the topic "Stress distribution around a circular hole"

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Cai, Ming-Hong, and 蔡明宏. "Stress Distribution in Composite Plates with a Circular Hole." Thesis, 2014. http://ndltd.ncl.edu.tw/handle/50053215901833466969.

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碩士<br>義守大學<br>土木與生態工程學系<br>102<br>The effect of various off­axis angles and lamina material properties on the stress distribution of a circular cutout in an orthotropic composite plate under off-axis loading is presented. Based on the generalized Hooke’s law and the complex variable method, a dimensionless analysis is used to evaluate the influence of various elastic moduli E1, E2, G12 and ν12 on the stress distribution along the boundary of the circular cutout under various off-axis loadings. The results obtained from this dimensionless analysis provide a set of general design guidelines for
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Books on the topic "Stress distribution around a circular hole"

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Facility, Dryden Flight Research, ed. Stress concentration around a small circular hole in the HiMAT composite plate. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

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2

Facility, Dryden Flight Research, ed. Temperature effect on stress concentration around circular hole in a composite material specimen representative of X-29A forward-swept wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1989.

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Facility, Dryden Flight Research, ed. Stress concentration around circular hole in a composite material specimen representative of the X-29A forward-swept wing aircraft. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

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National Aeronautics and Space Administration (NASA) Staff. Temperature Effect on Stress Concentration Around Circular Hole in a Composite Material Specimen Representative of X-29a Forward-Swept Wing Aircraft. Independently Published, 2018.

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Book chapters on the topic "Stress distribution around a circular hole"

1

Fernandes, José Luiz, Antonio Carlos Marques Alvim, and Renato Seixas da Rocha. "A Proposal of Strain-Gage Rosette for Measurement Residual Stress Around a Circular Hole in a Plate With Circular Hole." In III European Conference on Computational Mechanics. Springer Netherlands, 2006. http://dx.doi.org/10.1007/1-4020-5370-3_64.

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Mohammed Shafeeque, Kannan Kulavan, and K. V. N. Surendra. "Stress Distribution in Infinitely Long Plate with Circular Hole Loaded by Concentrated Loads." In Recent Advances in Applied Mechanics. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-9539-1_7.

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Mindlin, Raymond D. "Stress Distribution Around a Hole Near the Edge of a Plate under Tension." In The Collected Papers of Raymond D. Mindlin Volume I. Springer New York, 1989. http://dx.doi.org/10.1007/978-1-4613-8865-4_20.

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4

Nakano, Y., F. Nakagawa, and T. Sawa. "Thermal Stress Distribution in Butt Adhesive Joints Having a Circular Hole in an Adhesive." In Fracture of Engineering Materials and Structures. Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3650-1_56.

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Badiger, Shrikrishna, and D. S. Ramakrishna. "Stress Distribution in an Infinite Plate with Circular Hole by Modified Body Force Method." In Lecture Notes on Multidisciplinary Industrial Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-3254-2_16.

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Bao-Ju, Yun, Cheng Yuan-Ping, and Zhou Hong-Xing. "Numerical Simulation on Deformation and Stress Distribution around Spraying Hole in Outburst Coal Seam." In Proceedings of the 2012 International Conference on Communication, Electronics and Automation Engineering. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-31698-2_84.

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Hudramovich, Vadym, Eteri Hart, and Bohdan Terokhin. "Stress Concentration Around a Circular Hole in Thin Plates and Cylindrical Shells with a Radially Inhomogeneous Inclusion." In Selected Problems of Solid Mechanics and Solving Methods. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-54063-9_18.

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Anand, Lallit, Ken Kamrin, and Sanjay Govindjee. "Stress concentration." In Introduction to Mechanics of Solid Materials. Oxford University PressOxford, 2022. http://dx.doi.org/10.1093/oso/9780192866073.003.0008.

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Abstract This chapter considers the concentration of stress around a circular hole in a large plate. The two canonical problems of far-field radial loading and far-field tension are considered in detail. For both cases, cylindrical coordinates are employed to develop the solutions. These two cases are illustrative of the general concept of stress concentration and stress concentration factor—a concept which is further discussed for an elliptical crack-like defect in a plate under far-field tension. The role of such stress concentration sites as places at which a crack can nucleate and cause fr
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Serafinavičius Tomas, Šaučiuvėnas Gintas, and Hildebrand Jörg. "Stress Distribution of Tension Structural Glass Plates." In Challenging Glass 3. IOS Press, 2012. https://doi.org/10.3233/978-1-61499-061-1-565.

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This paper deals with the results received by carried out tensile tests of the structural glass plates supplied with three different types of stress raisors. The first type of specimens is the plate with a circular hole located in the centre of the plate, the second one is the plate with a slot hole located in the centre of the plate, and the third one is the plate with the semicircular notches located at the opposite edges. The results of test of these specimens were compared both among themselves and both with the results of the specimens without stress raisors. The specimens were made from
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Ting, T. T. C. "Anisotropic Materials with an Elliptic Boundary." In Anisotropic Elasticity. Oxford University Press, 1996. http://dx.doi.org/10.1093/oso/9780195074475.003.0013.

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The determination of stress distribution in a solid with the presence of a hole or an inclusion has been a mathematically interesting and challenging problem. It is also an important problem in applications. The simplest geometry of the hole is a circle. For isotropic materials a hole of arbitrary shape can be transformed, in theory, to a circle by a conformal mapping (Muskhelishvili, 1953; see also Section 3.12). Therefore a circular hole is all one needs to study for isotropic materials. For anisotropic materials there are three complex variables ɀα=x1+pαx2 (α=1,2,3). It is in general not po
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Conference papers on the topic "Stress distribution around a circular hole"

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Gultekin, Ece, Berkay Ozkan, and Evren Eyup Taskinoglu. "Machine Learning Based Stress Prediction Around the Hole of Attachment Lug Structures for Flaw Tolerance Evaluations." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-203.

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This study investigates the stress concentration and damage tolerance of lug structures, with an application example using the horizontal tail plane lug of a light utility helicopter. Using Finite Element Analysis (FEA), stress distributions around the lug hole were simulated under varying load conditions to understand how different loading angles and magnitudes affect stress concentrations. A machine learning approach was employed to predict stress distributions based on a dataset generated from FEA simulations. Several regression models were tested and Random Forest Regression model yields t
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Aluko, O., and H. A. Whitworth. "Contact Stress Analysis Around Elliptic Pin-Loaded Holes in Orthotropic Plates." In ASME 2010 International Mechanical Engineering Congress and Exposition. ASMEDC, 2010. http://dx.doi.org/10.1115/imece2010-37662.

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This analysis utilizes the complex stress function approach to obtain the stress distribution in pin loaded composite joints with elliptic openings. The stress functions were derived from assumed displacement expressions that satisfy the boundary conditions around the hole. In the method of solution Coulomb friction was used to determine the prescribed displacements at the boundary. The material properties of graphite/epoxy and carbon fiber reinforced plastics laminates were used in this investigation and the results also compared with available data for joints with circular openings. It was r
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Yavari, Vahid, Farshad Daneshvar, Mohammad-Hassan Kadivar, and Iraj Rajabi. "Design Parameters Effect on Load Distribution Around the Hole in Mechanically Fastened Pinned Connections." In ASME 2008 Pressure Vessels and Piping Conference. ASMEDC, 2008. http://dx.doi.org/10.1115/pvp2008-61021.

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The pinned connection is a principal joining element in many structures. In this article, we present two-dimensional stress analyses for isotropic plate with a pinned circular hole. A study of the pin and the plate material dissimilarity was done by Iyer [6] but still different aspects of the problem are remained to be mentioned. In this work different issues of mechanical engineering interests such as stress distribution in contact area and the magnitude and location of maximum contact pressure and tangential stress are computed with the aid of commercial software ABAQUS 6.6-1 finite element
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Yang, Quan-quan, Cun-Fa Gao, and Wen-Tao Chen. "Stress concentration around a circular hole in a functionally graded material finite plate." In 2011 Symposium on Piezoelectricity, Acoustic Waves, and Device Applications (SPAWDA 2011). IEEE, 2011. http://dx.doi.org/10.1109/spawda.2011.6167218.

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Kobayashi, Isao, and Mitsutoshi Nakajima. "Microchannel Emulsification Devices for Generating Highly Uniform Droplets." In ASME 2009 7th International Conference on Nanochannels, Microchannels, and Minichannels. ASMEDC, 2009. http://dx.doi.org/10.1115/icnmm2009-82138.

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Monodisperse emulsions consisting of uniform droplets have received a great deal of attentions over the past decade due to their high-tech applications, e.g., monodisperse microparticles as spacers for electronic devices and monodisperse micro-carriers for drug delivery systems (DDS). Our group proposed microchannel (MC) emulsification, which enables generating highly uniform droplets with the smallest coefficient of variation of below 5% using MC arrays of unique geometry. The resultant droplet size can be precisely controlled by MC geometry. Droplet generation for MC emulsification is very m
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Tandon, G. P., and R. Y. Kim. "Non-Destructive Evaluation of Damage Around Circular Holes in Bolted Composite Laminates." In ASME 2006 International Mechanical Engineering Congress and Exposition. ASMEDC, 2006. http://dx.doi.org/10.1115/imece2006-14987.

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One of the more formidable problems in composite research is the study of delamination and other failure modes in the vicinity of a circular hole in a laminate, e.g., a circular cut-out in a structure. In this problem, the singularity varies around the periphery of the hole as well as through the thickness of the laminate. Under tensile loading, the early failure modes in this problem consist of transverse cracks in various layers, so that delamination occurs only after other damage is precipitated, followed by fiber breakage leading to failure. A literature review of past work clearly shows t
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Sekihara, M., and T. Machida. "Optimization of Rotor Disk Shape Considering Equalization of Residual Stress Distribution Around Central Hole." In ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/99-gt-231.

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A method for optimizing a rotor disk shape so that it equalizes the residual stress distribution around the central hole has been developed. The shape around the central hole is considered a variable, and it is changed in order to determine the optimum for reducing the equivalent stress of the central hole. As a result, the optimized shape that equalizes the residual stress distribution to within 23% variation was found. Second, experiments with aluminum rotors verified the effectiveness of the optimized shape by measuring residual deformations and stresses. And it was confirmed that the measu
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Cruse, Michael W., Ushio M. Yuki, and David G. Bogard. "Investigation of Various Parametric Influences on Leading Edge Film Cooling." In ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-gt-296.

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Film cooling adiabatic effectiveness of a simulated turbine airfoil leading edge was studied experimentally. The leading edge had two rows of holes, one at nominally the stagnation line position and the second a few hole diameters downstream. Hole positions at the leading edge, and inclination of the holes with respect to the surface, were different than typically used in previous studies, but were representative of current design practice. Various leading edge film cooling parameters were investigated including stagnation line position, free-stream turbulence level, leading edge geometry, and
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Tandon, G. P., and R. Y. Kim. "Multi-Sensor Approach to Non-Destructive Evaluation of Damage Around Circular Holes in Composite Laminates." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-79275.

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One of the more formidable problems in composite research is the study of delamination and other failure modes in the vicinity of a circular hole in a laminate, e.g., a circular cut-out in a structure. In this problem, the singularity varies around the periphery of the hole as well as through the thickness of the laminate. Under tensile loading, the early failure modes in this problem consist of transverse cracks in various layers, so that delamination occurs only after other damage is precipitated, followed by fiber breakage leading to failure. A literature review of past work clearly shows t
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10

Yavari, Vahid, Iraj Rajabi, and Mohammad Hassan Kadivar. "The Effect of Friction on Load Distribution Around the Hole in Composite Pinned Connections." In ASME 2007 Pressure Vessels and Piping Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/pvp2007-26384.

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This paper presents analyses for computing and evaluating the behavior of the laminated composite plate at the contact area in single lap, mechanically fastened joints. The analyses involve three dimensional finite element models performed by ABAQUS 6.4-PR11 code to evaluate the stress distribution in contact surface, separation angle, the magnitude and location of maximum radial stress. Results are determined for quasi-isotropic model and attempts are made to validate the models with previous works. The variations of separation angles through the thickness are investigated and effects of fric
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