Relevant bibliographies by topics / Laminated composite cylinder

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

Academic literature on the topic 'Laminated composite cylinder'

Author: Grafiati
Published: 3 June 2025
Last updated: 31 July 2025

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Journal articles on the topic "Laminated composite cylinder"

1

Teshnizi, S. H. Sharifi, S. S. R. Koloor, G. Sharifishourabi, Amran Bin Ayob, and Yahya Mohd Yazid. "Effect of Ply Thickness on Displacements and Stresses in Laminated GFRP Cylinder Subjected to Radial Load." Advanced Materials Research 488-489 (March 2012): 367–71. http://dx.doi.org/10.4028/www.scientific.net/amr.488-489.367.

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The superior feature of composites such as high stiffness against low density have impelled engineers to use this material in automotive, aerospace and building industries. In the past few decades, composites shell has found applications in storage tanks and transmission pipelines. Designing laminated composite shells is challenging because of the complex mechanical behavior when combining laminate and shell theories. In this paper, the study is focused on the effect of lamina thickness on performance of the GFRP cylinder. For this purpose two 12-ply GFRP cylinders are considered with ply sequ
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Rattanawangcharoen, N., A. H. Shah, and S. K. Datta. "Reflection of Waves at the Free Edge of a Laminated Circular Cylinder." Journal of Applied Mechanics 61, no. 2 (1994): 323–29. http://dx.doi.org/10.1115/1.2901448.

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A wave function expansion method is employed to solve the reflection problem of time-harmonic elastic waves incident upon the free edge of a semi-infinite laminated circular cylinder. Wave functions are obtained using a propagator matrix approach for laminated isotropic cylinders and by a Rayleigh-Ritz type approximation for laminated composite cylinders. The least-square technique as well as the variational method are employed to evaluate the complex amplitudes and the energy flux associated with the reflected waves. To validate the solutions and present algorithm, results are compared with a
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Serhat, Gokhan. "Design of Circular Composite Cylinders for Optimal Natural Frequencies." Materials 14, no. 12 (2021): 3203. http://dx.doi.org/10.3390/ma14123203.

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This study concerns optimizing the eigenfrequencies of circular cylindrical laminates. The stiffness properties are described by lamination parameters to avoid potential solution dependency on the initial assumptions of the laminate configurations. In the lamination parameter plane, novel response contours are obtained for the first and second natural frequencies as well as their difference. The influence of cylinder length, radius, thickness, and boundary conditions on the responses is investigated. The lamination parameters yielding the maximum response values are determined, and the first t
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Rouhi, Mohammad, Hossein Ghayoor, Suong V. Hoa, and Mehdi Hojjati. "The effect of the percentage of steered plies on the bending-induced buckling performance of a variable stiffness composite cylinder." Science and Engineering of Composite Materials 22, no. 2 (2015): 149–56. http://dx.doi.org/10.1515/secm-2014-0258.

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AbstractThe fiber steering capability of automated fiber placement machines offers the designers more room to fully exploit the directional properties of composite materials. Circumferential stiffness tailoring by fiber steering can considerably increase the bending-induced buckling performance of laminated composite cylinders. The potential structural improvement resulting from fiber steering depends on different design parameters such as the number of plies considered for fiber steering in a laminate. In this study, the buckling performance improvement of a variable stiffness (VS) composite
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Ahmadi, Isa. "Edge stresses analysis in laminated thick sandwich cylinder subjected to distributed hygrothermal loading." Journal of Sandwich Structures & Materials 20, no. 4 (2016): 425–61. http://dx.doi.org/10.1177/1099636216657681.

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The boundary layer hygrothermal stresses in the thick sandwich cylinder with laminated face are investigated. Uniform and through the thickness steady-state distribution for temperature and moisture content can be considered in the analysis. A displacement based layer-wise formulation is presented for analysis of thick sandwich composite cylinders subjected to hygrothermal loading conditions. Considering a general displacement field and employing a displacement based layer-wise theory, the governing equations of thick laminated sandwich cylinder are obtained. The displacement based formulation
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Petreli, A. S., and N. G. Tsouvalis. "A Parametric Study of the Effect of Geometric Imperfections on the Buckling Behaviour of Composite Laminated Cylinders." Advanced Composites Letters 11, no. 3 (2002): 096369350201100. http://dx.doi.org/10.1177/096369350201100302.

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This paper presents the results of a parametric study about the type and magnitude of initial imperfections on the buckling behaviour of composite laminated cylinders under external hydrostatic load. Using the FE method, cylinders with two particular types of initial imperfections are non-linearly analysed. Results show that significant improvement of the cylinder buckling strength is observed when initial imperfections have a selected shape and magnitude, which induces a final cylinder deflected shape different from the modeshape of the geometrically perfect cylinder.
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Xi, Z. C., G. R. Liu, K. Y. Lam, and H. M. Shang. "A Strip Element Method for Analyzing Wave Scattering by a Crack in an Axisymmetric Cross-Ply Laminated Composite Cylinder." Journal of Applied Mechanics 67, no. 2 (1999): 427–29. http://dx.doi.org/10.1115/1.1303800.

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A strip element method is presented for analyzing waves scattered by a crack in an axisymmetric cross-ply laminated composite cylinder. The cylinder is at the outset discretized as axisymmetric strip elements through the radial direction. The application of the Hamilton variational principle develops a set of governing ordinary differential equations. The particular solutions to the resulting equations are found using a modal analysis approach in conjunction with the Fourier transform technique. The complementary solutions are formulated by the superposition of eigenvectors, the unknown coeffi
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Teshnizi, S. H. Sharifi, S. S. R. Koloor, G. Sharifishourabi, Amran Bin Ayob, and Yahya Mohd Yazid. "Mechanical Behavior of GFRP Laminated Composite Pipe Subjected to Uniform Radial Patch Load." Advanced Materials Research 488-489 (March 2012): 542–46. http://dx.doi.org/10.4028/www.scientific.net/amr.488-489.542.

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Cylindrical vessels are widely used for storage and transportation of fluids. Using composites shells can improve the corrosion resistance of the product and reduce weight therefore investigation of the mechanical behavior is important. For this purpose cylinders with 6, 12 and18-ply of GFRP , with symmetric ply sequence of [90/0/90]s, [90/0/90/0/90/0]s and, [90/0/90/0/90/0/90 /0/90]s with layer thickness 1.3 mm and mean radius 250 mm, are considered under uniform radial patch load. The analysis was based on the shell theory and classical mechanics of laminated composites. A code was written u
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SHAH, NAZIM SULTAN, and HARSHAL AHER. "Free Vibration Characteristics Investigation in Composite Laminated Open Cylindrical Shells." Mazedan Transactions on Engineering Systems Design 5, no. 2 (2024): 22–24. https://doi.org/10.5281/zenodo.14452000.

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The shell vibration problem is of continuing interest due to their rampant use as structural members. Often these shells are made of laminated composites. These laminated shells have a very wide range of applications, particularly in aerospace, military hardware, marine ships, and civil constructions, as well as an integral part of machines where they are subjected to dynamic loading hence their vibratory analysis, is important for efficient, reliable and failure-proof design. Composite laminated open shells in these applications are employed with various boundary conditions. Understanding the
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Хасанова, Г. А. "СОЗДАНИЕ МНОГОСЛОЙНОГО КОМПОЗИТА С ИСПОЛЬЗОВАНИЕМ УГЛЕРОДНЫХ ВОЛОКОН НА ОСНОВЕ МОДЕЛИ ВЫПУЧИВАНИЯ КОМПОЗИТНОГО ЦИЛИНДРА". ИЗВЕСТИЯ ВУЗОВ КЫРГЫЗСТАНА, № 3 (29 червня 2024): 3–8. https://doi.org/10.26104/ivk.2024.27.84.001.

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Высококачественные композиционные материалы ис­поль­зуются в различных областях науки и техники. Поиск лег­ких, прочных, теплопроводных и недорогих композитных ма­те­­риалов – это потребность времени. Композитные мате­риа­лы используются для снижения веса кораблей, транспорт­ных средств, строительных конструкций и самолетов. Ком­по­­зи­ционный материал из эпоксидной смолы из углеродного волокна обладает превосходной химической стойкостью и тер­мостойкостью. Еще одной характе­ристикой армирован­ных волокном материалов является свойство анизотропии. В последние годы большое внимание уделяется пр
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Dissertations / Theses on the topic "Laminated composite cylinder"

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Talbot, Casey A. "Axisymmetric Finite Element Modeling of Adhesive Joint Between a Laminated Composite and Metal Cylinder." DigitalCommons@USU, 2011. https://digitalcommons.usu.edu/etd/1080.

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In order to incorporate fiber-reinforced composite materials in space structures, adhesive joining techniques are required. Because analytical models have a hard time capturing the complex stress state inherent to adhesively joining dissimilar materials, a different modeling technique was deemed necessary. A two-dimensional axisymmetric finite element model capable of capturing the three-dimensional stress state of cylindrical adhesive joints was developed. In order to rigorously validate the model, testing was undergone to ensure the model accurately predicted joint displacements. Displacemen
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Zhuang, Wei. "Numerical modeling for elastodynamic problems in laminated composite cylinders." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1999. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp03/NQ35049.pdf.

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Kugler, Danielle. "Experimental investigation of the effect of changes in processing history on compositie laminates and cylinders /." Digital version accessible at:, 1998. http://wwwlib.umi.com/cr/utexas/main.

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Johnson, Wayne Michael. "Structural acoustic optimization of a composite cylindrical shell." Diss., Available online, Georgia Institute of Technology, 2004:, 2004. http://etd.gatech.edu/theses/available/etd-06072004-131213/unrestricted/johnson%5Fwayne%5Fm%5F200405%5Fphd.pdf.

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Zhuang, Wei. "Numerical modeling for elastodynamic problems in laminated composite cylinders." 1998. http://hdl.handle.net/1993/1609.

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Propagation and scattering of elastic waves in laminated composite cylinders are studied in this thesis. Axisymmetric steady-state elastodynamic Green's functions for laminated composite cylinders are constructed by the superposition of numerically generated modal solutions from an eigensystem, which is based on a semi-analytical finite element formulation. Boundary element method is employed to investigate scattering of waves due to circumferential flaws in laminated composite cylinders. Also, a hybrid method, which combines axisymmetric finite element modeling in an interior bounded region
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Books on the topic "Laminated composite cylinder"

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Butler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. National Aeronautics and Space Administration, 1989.

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Butler, Theresa Ann. The structural response of unsymmetrically laminated composite cylinders. National Aeronautics and Space Administration, 1989.

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3

United States. National Aeronautics and Space Administration., ed. Axisymmetric deformations and stresses of unsymmetrically laminated composite cylinders in axial compression with thermally-induced preloading effects. Carderock Division, Naval Surface Warfare Center, 1993.

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Hyer, M. W. Innovative design of composite structures: Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. College of Engineering, Virginia Polytechnic Institute and State University, 1990.

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Center, Langley Research, ed. An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders. National Aeronautics and Space Administration, Langley Research Center, 1988.

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Center, Langley Research, ed. An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders. National Aeronautics and Space Administration, Langley Research Center, 1988.

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National Aeronautics and Space Administration (NASA) Staff. Structural Response of Unsymmetrically Laminated Composite Cylinders. Independently Published, 2018.

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National Aeronautics and Space Administration (NASA) Staff. Innovative Design of Composite Structures: Axisymmetric Deformations of Unsymmetrically Laminated Cylinders Loaded in Axial Compression. Independently Published, 2018.

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An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders. National Aeronautics and Space Administration, Langley Research Center, 1988.

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Book chapters on the topic "Laminated composite cylinder"

1

Pagano, N. J. "Stress Gradients in Laminated Composite Cylinders." In Solid Mechanics and Its Applications. Springer Netherlands, 1994. http://dx.doi.org/10.1007/978-94-017-2233-9_13.

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MAEKAWA, I., H. SHIBATA, M. NAKAYAMA, and A. KOBAYASHI. "STRESS WAVE PROPAGATION BEHAVIOR IN LAMINATED COMPOSITE HOLLOW CYLINDER." In Mechanical Behaviour of Materials VI. Elsevier, 1992. http://dx.doi.org/10.1016/b978-0-08-037890-9.50064-8.

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"Characteristics of Waves in Composite Cylinders." In Elastic Waves in Anisotropic Laminates. CRC Press, 2001. http://dx.doi.org/10.1201/9781420040999.ch15.

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"Wave Scattering by Cracks in Composite Cylinders." In Elastic Waves in Anisotropic Laminates. CRC Press, 2001. http://dx.doi.org/10.1201/9781420040999.ch16.

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Conference papers on the topic "Laminated composite cylinder"

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Idan, Muayad Mohammed. "Low Velocity Impact Response of Laminated Composite Cylinder." In 2019 2nd International Conference on Engineering Technology and its Applications (IICETA). IEEE, 2019. http://dx.doi.org/10.1109/iiceta47481.2019.9012986.

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Anderson, Jacob P., and M. Cengiz Altan. "Properties of Composite Cylinders Fabricated by Bladder Assisted Composite Manufacturing (BACM)." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-65285.

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An innovative manufacturing method, BACM (Bladder Assisted Composite Manufacturing), to fabricate geometrically complex, hollow parts made of polymeric composite materials is presented. BACM uses an internally heated bladder to provide the consolidation pressure at the required cure temperature, and thus produces high quality components. The feasibility of this manufacturing method is demonstrated by fabricating laminated composite cylinders using multiple cure pressures and wall thicknesses. The mechanical properties, energy consumed during the curing, and void content of the composite cylind
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Katsuo, Masahide, Toshiyuki Sawa, Koji Kawaguchi, and Hiroshi Kawamura. "Axisymmetrical Thermal Stress Analysis of Laminated Composite Finite Hollow Cylinders Restricted at Both Ends in Steady State." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0860.

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Abstract The thermal stress distributions of laminated composite finite hollow cylinders restricted at both ends and at one end of the cylinders are analyzed using the thermoelastic displacement potential and Michell’s stress functions based on the axisymmetrical theory of elasticity. In the numerical calculations, the thermal stress distributions in the laminated composite finite hollow cylinders are examined. The effects of restrictions at the end of the cylinders on the thermal stress distributions are clarified. The analytical results are compared with the results obtained from the plain s
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Yousuf, Louay S. "Nonlinear Dynamics Investigation of Bending Deflection Of Stiffened Composite Laminated Plate Using Lyapunov Exponent Conception." In ASME 2021 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/imece2021-67448.

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Abstract In this paper, the nonlinear dynamics behavior of the bending deflection of stiffened composite laminated plate is investigated using largest Lyapunov exponent parameter. Wolf algorithm is used to quantify largest Lyapunov exponent in the presence of aspect ratios and fiber volume fractions. A power spectrum analysis has been added using the amplitude of Fast Fourier Transform (FFT) to detect the non-periodic motion of the stiffened plate. Numerical simulation is carried out using ANSYS software. The combined loading are the in-plane compression (uniaxial) mechanical load and shear fo
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Li, H. Y., H. Li, S. D. Hu, and Z. B. Chen. "Experiment on Active Vibration Isolation of a Conical Shell Isolator." In ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/imece2014-37850.

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Conical shells have advantages such as light weight, higher stiffness and strength, its stiffness ratio between axial and transverse directions can be easily adjusted by changing its apex angle. Thus conical shell can be utilized as an isolator to protect precision payloads and equipment from severe dynamic loads. In this study, vibration isolation performance of a conical shell isolator laminated with piezoelectric actuators is investigated. The conical shell isolator is manufactured from epoxy resin. The payload is at the minor of the isolator. The major end of the isolator is fixed at a fla
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Silva, Joao F., Joao P. Nunes, and Joao C. Velosa. "Using Thermoplastic (HDPE) Liners and Glass Fiber Reinforced Thermosetting and Thermoplastic Structural Wall Matrices to Produce Filament Wound Pressure Vessels." In ASME 2010 Pressure Vessels and Piping Division/K-PVP Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/pvp2010-25826.

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Polymer composites are an excellent alternative to replace more traditional materials in the fabrication of pressure cylinders for common applications. They minimize the weight and improve the mechanical, impact and corrosion behavior, which are relevant characteristics for almost all current and future large scale pressure cylinder applications, such as liquid filters and accumulators, hydrogen cell storage vessels, oxygen bottles, etc. A new generation of composite pressure vessels has been studied in this work. The vessels consist on a thermoplastic liner wrapped with a filament winding gla
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Xiao, J. R., B. A. Gama, and J. W. Gillespie. "Progressive Damage and Delamination in Plain Weave S-2 Glass/SC-15 Composites Under Quasi-Static Punch Shear Loading." In ASME 2005 International Mechanical Engineering Congress and Exposition. ASMEDC, 2005. http://dx.doi.org/10.1115/imece2005-82261.

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Quasi-static punch-shear tests are carried out on plain weave (PW) S-2 glass/SC-15 epoxy composite laminates with a right circular cylinder punch to identify the sequence and extent of damage and the corresponding displacements at which they occur for a wide range of laminate thicknesses. Two different support spans of 25.4 mm (1 in) and 101.6 mm (4 in) diameter with different layers (0.6 mm ply thickness) of composite laminates are tested under quasi-static loading to identify compression-shear and tension-shear dominated modes of damage. Numerical punch shear experiments are conducted using
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Kim, Ran Y., Allan S. Crasto, and Gregory A. Schoeppner. "Dimensional Stability of Composite in a Space Thermal Environment." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-1169.

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Abstract Composites are steadily replacing metals in weight-critical space structures primarily because of their high specific moduli. Many space structures require not only high stiffness but precision alignment and dimensional stability as well. These parameters are sensitive to thermal strains caused by the mismatch in coefficients of thermal expansion (CTE) of the constituents, anisotropy in ply CTE, and variations in service temperature. The CTE of a laminate can change in service as a result of mechanically or thermally induced microcracking and this may result in undesirable distortion
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FUCHS, HANNES, and MICHAEL HYER. "The nonlinear bending response of thin-walled laminated composite cylinders." In 33rd Structures, Structural Dynamics and Materials Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2230.

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Hyer, Michael W., and Jaret C. Riddick. "Displacement Response of Segmented-Stiffness Composite Cylinders." In ASME 1998 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/imece1998-1192.

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Abstract With advanced manufacturing technology such as tow placement devices and filament winders, cylindrical composite structures may well be constructed in such a fashion that the lamination sequence varies with circumferential location around the cylinder. For example, the stacking sequence at the top and bottom of the cylinder may be axially stiff to resist bending and axial loads, while the sides of the cylinder may be designed to resist shear loads. The variation in stacking sequence may be continuous, with the stacking sequences on the top and bottom making a smooth transition to anot
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Reports on the topic "Laminated composite cylinder"

1

Blake, H. W., and J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10151163.

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Blake, H. W., and J. M. Starbuck. Hydrostatic testing of thick laminated composite cylinders for performance model validation. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/6855310.

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