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The Nile on eBay Polymer Matrix Composites by R.E. Shalin This book gives the basic principles used to develop high-strength, high-modulus polymer composites, while considering a wide spectrum of parameters associated with such a task. FORMAT Hardcover LANGUAGE English CONDITION Brand New Publisher Description This book is part of a series dedicated to advanced composite materials, research, development and usage in the former Soviet Union. It provides the basic principles used to develop high-strength, high-modulus composites. Starting with types of matrix materials, the text progresses on to the development and production of fibrous composites, their structure-property relationships, hybrid composite materials, and the development of these materials in aerospace applications. It should be of interest to anyone researching or developing composite materials science and technology, both in industry and universities. Table of Contents Polymeric matrices in fibre-reinforced composite materials.- 1.1 Introduction.- 1.2 High-crosslink-density polymeric matrices.- 1.3 Matrices manufactured of thermostable linear and low-crosslinkdensity polymers.- References.- Some principles for creating fibrous composites with a polymeric matrix.- 2.1 Introduction.- 2.2 Compatibility of components and solidity of polymeric composites.- 2.3 Structural defects and mechanical properties of polymeric composites.- 2.4 Control over properties of composites by changing composition and structure.- References.- Structural carbon-fibre-reinforced plastics and their properties.- 3.1 Introduction.- 3.2 Components for structural carbon-fibre-reinforced plastics.- 3.3 Epoxy carbon-fibre-reinforced plastics.- 3.4 Carbon-fibre-reinforced plastics with thermoplastic matrix.- 3.5 Component properties and high-temperature strength of heatresistant carbon-fibre-reinforced plastics.- 3.6 Structure-simulating modelling of carbon-fibre-reinforced plastics with given tensile and compressive properties.- References.- Organoplastics.- 4.1 Reinforcing materials.- 4.2 Binders.- 4.3 Composites.- References.- Glass plastics.- 5.1 Introduction.- 5.2 Glass-fibre fillers.- 5.3 Binders of glass plastics.- 5.4 Properties of glass plastics.- 5.5 Glass plastics technology and applications.- References.- Hybrid composite materials.- 6.1 Introduction.- 6.2 Levels of hybridization and structure of hybrid composite materials.- 6.3 Calculation and design of hybrid composite materials.- 6.4 Production of hybrid composite materials and articles therefrom.- 6.5 Characteristic features and fields of application.- References.- Principles of developing organic-fibre-reinforced plastics for aircraft engineering.- 7.1 Introduction.- 7.2 Peculiarities of the propertiesof aramid fibres used as fillers for polymeric composites.- 7.3 Thermoreactive binders for organoplastics 320.- 7.4 Peculiarities of the physicochemical interaction of aramid fibres with the components of thermoreactive oligomeric binders 324.- 7.5 Peculiarities of thermoreactive binder curing in the presence of aramid fibres.- 7.6 Adhesive interaction in polymeric fibre-polymeric cured matrix systems.- 7.7 Relaxation processes in organoplastics.- 7.8 Mechanical properties of organic-fibre-reinforced plastics.- 7.9 Effect of water and its vapour on organoplastic properties.- 7.10 Dielectric properties of organoplastics.- 7.11 Thermal properties of organoplastics.- 7.12 Applications of organoplastics in aircraft engineering.- References. Review `... essential reading for anyone concerned with polymer-matrix composite.' TRIP Long Description Some years ago in Paisley (Scotland) the International Conference on Composite Materials, headed by Professor I. Marshall, took place. During the conference, I presented a paper on the manufacturing and properties of the Soviet Union's composite materials. Soviet industry had made great achievements in the manufacturing of composite materials for aerospace and rocket applications. For example, the fraction of composites (predominantly carbon fibre reinforced plastics) in the large passenger aircrafts Tu-204 and 11-86 is 12-15% of the structure weight. The percentage by weight share of composites in military aircraft is greater and the fraction of composites (organic fibre reinforced plastics) used in military helicopters exceeds a half of the total structure weight. The nose parts of most rockets are produced in carbon-carbon materials. In the Soviet spacecraft 'Buran' many fuselage tubes are made of boron-aluminium composites. Carbon-aluminium is used for space mirrors and gas turbine blades. These are just a few examples of applications. Many participants at the Paisley conference suggested that the substantial Soviet experience in the field of composite materials should be distilled and presented in the form of a comprehensive reference publication. So the idea of the preparation and publication of a six volume work Soviet Advanced Composites Technology, edited by Academician J. Fridlyander and Professor I. Marshall, was born. Review Quote '... essential reading for anyone concerned with polymer-matrix composite.' TRIP Details ISBN 0412613301 Author R.E. Shalin Language English ISBN-10 0412613301 ISBN-13 9780412613302 Media Book Format Hardcover DEWEY 620.192 Series Number 4 Year 1995 Edited by R.E. Shalin Imprint Chapman and Hall Place of Publication London Country of Publication United Kingdom Short Title POLYMER MATRIX COMPOSITES 1995 Pages 440 Edition 1995th Illustrations 6 Illustrations, black and white; XIII, 440 p. 6 illus. DOI 10.1604/9780412613302;10.1023/b131499;10.1007/978-94-011-0515-6 AU Release Date 1995-03-31 NZ Release Date 1995-03-31 UK Release Date 1995-03-31 Publisher Chapman and Hall Edition Description 1995 ed. Series Soviet Advanced Composites Technology Series Publication Date 1995-03-31 Alternative 9789401042291 Audience Professional & Vocational We've got this At The Nile, if you're looking for it, we've got it. With fast shipping, low prices, friendly service and well over a million items - you're bound to find what you want, at a price you'll love! TheNile_Item_ID:96246737;