Mechanics of Aircraft Structures

C.T. Sun

320 pages, parution le 29/06/2006 (2^eme édition)

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Résumé

Designed to help students get a solid background in structural mechanics and extensively updated to help professionals get up to speed on recent advances

This Second Edition of the bestselling textbook Mechanics of Aircraft Structures combines fundamentals, an overview of new materials, and rigorous analysis tools into an excellent one-semester introductory course in structural mechanics and aerospace engineering. It's also extremely useful to practicing aerospace or mechanical engineers who want to keep abreast of new materials and recent advances. Updated and expanded, this hands-on reference covers:

Introduction to elasticity of anisotropic solids, including mechanics of composite materials and laminated structures
Stress analysis of thin-walled structures with end constraints
Elastic buckling of beam-column, plates, and thin-walled bars
Fracture mechanics as a tool in studying damage tolerance and durability

Designed and structured to provide a solid foundation in structuralmechanics, Mechanics of Aircraft Structures, Second Edition includesmore examples, more details on some of the derivations, and more sample problems to ensure that students develop a thorough understanding of the principles.

L'auteur - C.T. Sun

C. T. SUN, PHD, is the Neil A. Armstrong Distinguished Professor inthe School of Aeronautics and Astronautics at Purdue University in West Lafayette, Indiana, and the recipient of the 2004 Purdue University Research Award. Dr. Sun teaches composites, elasticity, fracture mechanics, and aircraft structures. He is a Fellow of both the American Institute of Aeronautics and Astronautics (AIAA), the American Society of Mechanical Engineers (ASME), and the American Society for Composites (ASC).

Sommaire

Characteristics of Aircraft Structures and Materials
Introduction to Elasticity
Torsion
Bending and Flexural Shear
Flexural Shear Flow in Thin-Walled Sections
Failure Criteria for Isotropic Materials
Elastic Buckling
Analysis of Composite Laminates

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Caractéristiques techniques

	PAPIER
Éditeur(s)	Wiley
Auteur(s)	C.T. Sun
Parution	29/06/2006
Édition	2^eme édition
Nb. de pages	320
Format	16 x 24
Couverture	Relié
Poids	590g
Intérieur	Noir et Blanc
EAN13	9780471699668
ISBN13	978-0-471-69966-8