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Titlebook: Composite Structures; I. H. Marshall Book 1981 Applied Science Publishers Ltd 1981 boundary layer.composite material.damage.elasticity.fat

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書目名稱Composite Structures
編輯I. H. Marshall
視頻videohttp://file.papertrans.cn/232/231830/231830.mp4
圖書封面Titlebook: Composite Structures;  I. H. Marshall Book 1981 Applied Science Publishers Ltd 1981 boundary layer.composite material.damage.elasticity.fat
描述The papers contained herein were presented at the First International Conference on Composite Structures held at Paisley College of Technology, Paisley, Scotland, in September 1981. This conference was organised and sponsored by Paisley College of Technology in association with The Institution of Mechanical Engineers and The National Engineering Laboratory (UK). There can be little doubt that, within engineering circles, the use of composite materials has revolutionised traditional design concepts. The ability to tailor-make a material to suit prevailing environmental conditions whilst maintaining adequate reinforcement to withstand applied loading is unquestionably an attractive proposition. Significant weight savings can also be achieved by virtue of the high strength-to-weight and stiffness-to-weight characteristics of, for example, fibrous forms of composite materials. Such savings are clearly of paramount importance in transportation engineering and in particular aircraft and aerospace applications. Along with this considerable structural potential the engineer must accept an increased complexity of analysis. All too often in the past this has dissuaded the designer from consi
出版日期Book 1981
關(guān)鍵詞boundary layer; composite material; damage; elasticity; fatigue; finite element method; fracture; material;
版次1
doihttps://doi.org/10.1007/978-94-009-8120-1
isbn_softcover978-94-009-8122-5
isbn_ebook978-94-009-8120-1
copyrightApplied Science Publishers Ltd 1981
The information of publication is updating

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,Engineering Plastics—Some Factors Affecting Technology Transfer,y with parts that work but also with sufficient design technology for his continuing use of that material in like applications. The higher the design stresses and risk the greater is the quantity and quality of technology demanded. Since with many of today’s composite materials much of this technolo
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Stress and Strength Analysis of Bolted Joints in Composite Laminates,ile loading conditions. This investigation has been carried out within the framework of laminated plate theory. A finite element method has been utilized to conduct the stress analysis of the laminate with a loaded fastener hole. For this case the hole is assumed to be filled with a rigid core, simu
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Some Environmental and Geometric Effects on the Static Strength of Graphite Cloth Epoxy Bolted Joinposed by Hart-Smith. Among the variables covered were the amount of absorbed moisture in the laminates, their layup, bolt spacing, multiple bolt rows, single and double lap configurations. Tension shear testing was conducted at room temperature, 394 K (250°F), and 427K (310°F) to assess the impact o
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The Stress-Rupture Behaviour of GRP Laminates in Aqueous Environments,reep-rupture testing is in progress at Bath University, funded jointly by CEGB and Scott Bader Co. Ltd..The paper describes the background and aims of the work and gives details of the test programme and equipment, including a cell for single-sided exposure of a tensile testpiece. The behaviour of a
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