Analysis Of Composite Laminates Under UD Loads Using CLPT: Second Edition - Couverture souple

Vasamsetti, Subrahmanyam ; Geeri, Satish

9786209182778: Analysis Of Composite Laminates Under UD Loads Using CLPT: Second Edition

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ISBN 10 : 6209182771 ISBN 13 : 9786209182778

Editeur : LAP LAMBERT Academic Publishing, 2025

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�diteur: LAP LAMBERT Academic Publishing
Date d'�dition: 2025
Langue: anglais
ISBN 10: 6209182771
ISBN 13: 9786209182778
Reliure: Broch�
Nombre de pages: 60
Coordonn�es du fabricant: non disponible
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Analysis Of Composite Laminates Under UD Loads Using CLPT

Subrahmanyam Vasamsetti

Edit� par LAP LAMBERT Academic Publishing Nov 2025, 2025

ISBN 10 : 6209182771 ISBN 13 : 9786209182778

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Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 60 pp. Englisch. N� de r�f. du vendeur 9786209182778

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Analysis Of Composite Laminates Under UD Loads Using CLPT : Second Edition

Subrahmanyam Vasamsetti

Edit� par LAP LAMBERT Academic Publishing, 2025

ISBN 10 : 6209182771 ISBN 13 : 9786209182778

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Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne

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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The term composite can be defined as a combination of two or more dissimilar materials having a distinct interface between them such that the prosperities of the resulting material are superior to the individual constituent components. A composite laminate is two or more laminae bonded together to act as an integral structural element. Laminae principal material directions are oriented to produce a structural element capable of resisting load in several directions. From the analysis it is found that as the number of layers of a laminate increases in a given thickness, the strength of the laminate increases. It is also found that the location and angles of the principle material direction effect the strength of rectangular laminate, but it is not affecting the strength of a square laminate plate. On the application of the lateral load the outside laminae are subjected to higher stress than inner laminae and first ply failure occurs in outside laminae then to inside laminae. N� de r�f. du vendeur 9786209182778

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Analysis Of Composite Laminates Under UD Loads Using CLPT

Subrahmanyam Vasamsetti

Edit� par LAP LAMBERT Academic Publishing Nov 2025, 2025

ISBN 10 : 6209182771 ISBN 13 : 9786209182778

Neuf Taschenbuch

impression � la demande

Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne

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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -The term composite can be defined as a combination of two or more dissimilar materials having a distinct interface between them such that the prosperities of the resulting material are superior to the individual constituent components. A composite laminate is two or more laminae bonded together to act as an integral structural element. Laminae principal material directions are oriented to produce a structural element capable of resisting load in several directions. From the analysis it is found that as the number of layers of a laminate increases in a given thickness, the strength of the laminate increases. It is also found that the location and angles of the principle material direction effect the strength of rectangular laminate, but it is not affecting the strength of a square laminate plate. On the application of the lateral load the outside laminae are subjected to higher stress than inner laminae and first ply failure occurs in outside laminae then to inside laminae.VDM Verlag, Dudweiler Landstra�e 99, 66123 Saarbr�cken 60 pp. Englisch. N� de r�f. du vendeur 9786209182778

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