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9783659234811: Finite element modeling of composites and sandwich laminates: Modeling of composites and sandwich laminates using Finite element method

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a.INTRODUCTION The rapid increase in the industrial use of the advanced composite materials (Fibre Reinforced Laminated Composites) is considered as one of the important development in recent past. Better performance of these composite materials over conventional metallic materials has encouraged their use as structural materials in a wide range of engineering applications all over the world. b. ABSTRACT Laminated composites and sandwich plates have been widely used in civil, mechanical, aerospace, marine and other branches of engineering due to their high strength/stiffness to weight ratio and good tailoring capability compared to the conventional materials. However, laminated composite materials are weak in shear due to its low shear modulus compared to extensional rigidity. This phenomenon is quite significant in case of laminated sandwich plates due to wide variation of materials between the core and face sheets. . APPLICATIONS 1. Aerospace Engineering 2. Mechanical Engineering 3. Civil Engineering

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About the AuthorSushil Kumar Singh presently serves as a Assistant professor in the Department of Civil Engineering at School of Engineering, Shiv Nadir University Dadri U. P., India. Prior to this appointment Singh was a research fellow at India Institute of Technology Roorkee, Roorkee Uttrakhand, India for pursuing Phd degree.

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Sushil Kumar Singh, Anupam Chakrabarti
Publicado por LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659234818 ISBN 13: 9783659234811
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Condición: Sehr gut. Zustand: Sehr gut | Seiten: 200 | Sprache: Englisch | Produktart: Bücher. Nº de ref. del artículo: 22863100/2

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SUSHIL KUMAR SINGH|Anupam Chakrabarti
Publicado por LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659234818 ISBN 13: 9783659234811
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Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: SINGH SUSHIL KUMARAbout the AuthorSushil Kumar Singh presently serves as a Assistant professor in the Department of Civil Engineering at School of Engineering, Shiv Nadir University Dadri U. P., India. Prior to this appointment Singh. Nº de ref. del artículo: 5141859

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Sushil Kumar Singh
ISBN 10: 3659234818 ISBN 13: 9783659234811
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Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -a.INTRODUCTION The rapid increase in the industrial use of the advanced composite materials (Fibre Reinforced Laminated Composites) is considered as one of the important development in recent past. Better performance of these composite materials over conventional metallic materials has encouraged their use as structural materials in a wide range of engineering applications all over the world. b. ABSTRACT Laminated composites and sandwich plates have been widely used in civil, mechanical, aerospace, marine and other branches of engineering due to their high strength/stiffness to weight ratio and good tailoring capability compared to the conventional materials. However, laminated composite materials are weak in shear due to its low shear modulus compared to extensional rigidity. This phenomenon is quite significant in case of laminated sandwich plates due to wide variation of materials between the core and face sheets. . APPLICATIONS 1. Aerospace Engineering 2. Mechanical Engineering 3. Civil Engineering 200 pp. Englisch. Nº de ref. del artículo: 9783659234811

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Sushil Kumar Singh
Publicado por LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659234818 ISBN 13: 9783659234811
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Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - a.INTRODUCTION The rapid increase in the industrial use of the advanced composite materials (Fibre Reinforced Laminated Composites) is considered as one of the important development in recent past. Better performance of these composite materials over conventional metallic materials has encouraged their use as structural materials in a wide range of engineering applications all over the world. b. ABSTRACT Laminated composites and sandwich plates have been widely used in civil, mechanical, aerospace, marine and other branches of engineering due to their high strength/stiffness to weight ratio and good tailoring capability compared to the conventional materials. However, laminated composite materials are weak in shear due to its low shear modulus compared to extensional rigidity. This phenomenon is quite significant in case of laminated sandwich plates due to wide variation of materials between the core and face sheets. . APPLICATIONS 1. Aerospace Engineering 2. Mechanical Engineering 3. Civil Engineering. Nº de ref. del artículo: 9783659234811

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Sushil Kumar Singh
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Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -a.INTRODUCTION The rapid increase in the industrial use of the advanced composite materials (Fibre Reinforced Laminated Composites) is considered as one of the important development in recent past. Better performance of these composite materials over conventional metallic materials has encouraged their use as structural materials in a wide range of engineering applications all over the world. b. ABSTRACT Laminated composites and sandwich plates have been widely used in civil, mechanical, aerospace, marine and other branches of engineering due to their high strength/stiffness to weight ratio and good tailoring capability compared to the conventional materials. However, laminated composite materials are weak in shear due to its low shear modulus compared to extensional rigidity. This phenomenon is quite significant in case of laminated sandwich plates due to wide variation of materials between the core and face sheets. . APPLICATIONS 1. Aerospace Engineering 2. Mechanical Engineering 3. Civil EngineeringBooks on Demand GmbH, Überseering 33, 22297 Hamburg 200 pp. Englisch. Nº de ref. del artículo: 9783659234811

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Singh, Sushil Kumar, Chakrabarti, Anupam
Publicado por LAP LAMBERT Academic Publishing, 2012
ISBN 10: 3659234818 ISBN 13: 9783659234811
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